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First published on Friday, Mar 28, 2025 and last modified on Thursday, Apr 10, 2025 by François Chaplais.

Confinement to deterministic manifolds and low-dimensional solution formulas for continuously measured quantum systems
arXiv
Published version: 10.48550/arXiv.2503.08296

Alain Sarlette Laboratoire de Physique de l’Ecole normale supérieure, ENS-PSL, CNRS, Inria, Centre Automatique et Systèmes (CAS), Mines Paris, Université PSL, Sorbonne Université, Université Paris Cité, Paris, France; and Dptmt. Electronics and Information Systems, Ghent University, Belgium. Email

Cyril Elouard Université de Lorraine, CNRS, LPCT, F-54000 Nancy, France

Pierre Rouchon Laboratoire de Physique de l’Ecole normale supérieure, ENS-PSL, CNRS, Inria, Centre Automatique et Systèmes (CAS), Mines Paris, Université PSL, Sorbonne Université, Université Paris Cité, Paris, France.

Abstract

Quantum systems under continuous weak measurement follow stochastic differential equations (SDE). Depending on the stochastic measurement results indeed, the quantum state can progressively diffuse, a priori in all directions of state space. This note draws attention to the observation that, in several settings of interest for quantum engineering, this diffusion in fact takes place in low dimension. Namely, the state remains confined in a low-dimensional nonlinear manifold, often time-dependent, but independent of the measurement results. The note provides the corresponding low-dimensional expressions for computing the stochastically evolving state in several such settings: quantum non-demolition measurement in arbitrary dimensions; quadrature measurements on a harmonic oscillator (linear quantum system); and subsystem measurement in multi-partite quantum systems. An algebraic criterion is proposed to directly check when such low-dimensional manifolds exist or survive under additional dynamics.

1 Introduction

The wavefunction collapse under projective measurements is one of the most prominent features of quantum systems [1, 2, 3]. For more general measurement processes, the update of the wavefunction \( |\psi_t\rangle\) , or of the density operator \( \rho_t\) , conditioned on measurement results, follows the usual rules of conditional dynamics or filtering [4, 5]. In the continuous-time measurement limit, the resulting equations are known under various names like Belavkin filter, quantum trajectories, or stochastic master equation, see [6, 7] for instance. The associated “quantum trajectory” solution \( \rho_t(y)\) describes the density operator governing the probability distribution of any observable at time \( t\) , conditioned on an initial state \( \rho_0\) , on known system dynamics (Hamiltonian, decoherence channels, measurement channels), and on the measurement results \( y\) over the time interval \( [0,t)\) . This is the most natural filter for real-time operation, and the focus of the present note. Other filters include e.g. the past quantum state filter [8, 9, 10], which gives \( \rho_t\) conditioned on measurement results over \( [0,T] \ni t\) . The latter can be used e.g. in post-processing for experiment characterization; when an evolving ancilla is supposed to inform about a system with which it has interacted in the past; or with \( t=0\) , for estimating an initial state.

For continuous-time weak measurement processes as considered in the present note, \( \rho_t\) follows a nonlinear stochastic differential master equation (SDE, see [11, 12, 13, 14, 15]). The stochastic part reflects the measurement results; a posteriori, i.e. for a given measurement signal \( y\) over \( [0,t]\) , the equation can be integrated explicitly to obtain a state \( \rho_t(y)\) . However, when facing the equation a priori, trying to predict where the system can go in the near future, we are facing a probability distribution over possible trajectories. Sampling from all these possibilities implies a huge increase in complexity e.g. for numerical simulation or for system and control design. The (Gorini–Kossakowski–Sudarshan-) Lindblad master equation [16, 17, 18] is deterministic, linear and represents the average system evolution. It predicts the distribution of future measurement outcomes when not conditioning on intermediate measurements. However, as soon as one would apply control depending on measurement results [19, 20, 21, 22, 23, 24], or study time-correlations or purity of the density operator [25, 26] which are nonlinear functions of \( \rho_t\) , a more detailed description of the distribution over possible trajectories becomes necessary. A priori, a system following an SDE diffuses in all directions of its state space, independently of the number of stochastic processes affecting it. To keep trajectory prediction scalable in this context, efficient model reduction methods are necessary. For instance, in [27, 28], it is proposed to drastically reduce the dimension of a quantum filter, by developing the state at each time over a small number of selected basis states; the efficient choice of basis states then depends on a good a priori estimate of where the quantum state would go with high probability. A similar model reduction could also be the key for efficient “likely trajectory” estimation [29] and its applications, on high-dimensional quantum systems.

The present note underlines how such a priori model reduction works exactly, for several SDE models of particular interest in quantum engineering. More precisely, for those quantum systems, there exist nonlinear manifolds of low dimension, which evolve deterministically in time, and on which the trajectories remain confined for all possible measurement results. Only the movement along the manifold depends on the measurement results. In system-theoretic terms, we compute a minimal system representation, much smaller than \( \rho(t)\) , which still exactly models all output signal distributions for all initial conditions.

Regarding previous work, our attention has been drawn to the topic when observing manifolds in the experimental data of [30]. A corresponding full characterization of the qubit case is provided in [31] and the aim of the present note is to apply this analysis to higher-dimensional systems. In [32], the same property appears in the backwards equation for the past quantum state filter. The existence of such manifolds depends on an interplay between the measurement process(es) and the deterministic dynamics of the system, which can be checked with a systematic algebraic criterion. This general approach is shared with other recent work on exact quantum model reduction like [33, 34]. While the latter papers analyze structural properties for reduced quantum evolution, conditioned on initial conditions and observables of interest, the specificity of the present note is to provide reduced models which model all possible observables, once any initial condition has been fixed. Of course, this is only possible in even more particular cases; however, it is notable how typical building blocks of quantum engineering do feature this property.

The remainder of this note is organized as follows. Section 2 recalls the mathematical tools: quantum filter SDE, algebraic criterion for investigating confining manifolds. Section 3 summarizes the results for three applications:

  • quantum non-demolition measurements (QND) of a set of commuting observables;
  • some so-called linear quantum systems on the harmonic oscillator Hilbert space;
  • multi-partite quantum systems, covering mostly bipartite settings where a subsystem subject to a measurement process features Hamiltonian coupling to another subsystem.

The confinement onto low-dimensional manifolds is intimately linked to the existence of low-dimensional formulas for expressing the state as a function of the measurement results. Conversely, when the state diffuses in all directions as a function of the measurement history, it seems much less likely that a simple explicit formula would be able to express its solution. The appendix contains such explicit formulas, for a set of concrete instances of the three applications mentioned above.

Altogether, besides the technical formulas, the note mainly puts forward how useful the algebraic criterion turns out to be towards identifying drastic model reduction possibilities, and when they break down, in typically used quantum systems.

2 Catching deterministic manifolds: general method

A weak continuous-time measurement can be physically pictured as measuring a traveling electromagnetic wave, behind its weak interaction with the quantum system of interest. Monitoring the wave with photodetectors would lead to a stochastic equation featuring discrete jumps, i.e. a Poisson process [35, 36]. This note rather focuses on continuous monitoring of the wave amplitude, as theorized in [37, 11, 12, 13, 14, 15], and realized e.g. in [38, 39, 30] and routinely afterwards. Each measurement channel is associated to an operator \( L_k\) acting on the Hilbert space \( \mathcal{H}\) of the system of interest. The evolution of density operator \( \rho_t\) on \( \mathcal{H}\) , conditioned on the measurement results up to \( t\) , follows a stochastic differential equation in Itō sense [7, 15]:

\[ \begin{eqnarray} d\rho_t &=& -i\, [H, \rho_t]\, dt \end{eqnarray} \]

(1)

\[ \begin{eqnarray} && + \sum_{k=1}^{\bar k} \left(L_k \rho_t L_k^† - \tfrac{1}{2} (L_k^† L_k \rho_t + \tfrac{1}{2} \rho_t L_k^† L_k) \right) dt \\ \nonumber && + \sum_{k=1}^{\bar k} \left(L_k \rho_t + \rho_t L_k^† -\text{Tr}(L_k \rho_t + \rho_t L_k^†)\rho_t \right) \sqrt{\eta_k} \, dw_{t,k} \\ \nonumber &=:& -i\, [H, \rho_t]\, dt + \sum_{k=1}^{\bar k} F_{L_k}(\rho_t)\, dt \\ \nonumber && + \sum_{k=1}^{\bar k} G_{L_k}(\rho_t) \, \sqrt{\eta_k} \, dw_{t,k} \;\; ; \\ \nonumber dy_{t,k} &=& \sqrt{\eta_k}\, \text{Tr}(L_k \rho_t + \rho_t L_k^†)\, dt + dw_{t,k} \; \text{ for } k=1,2,...,{\bar k}. \\\end{eqnarray} \]

Here \( H\) denotes the system Hamiltonian, \( \eta_k \in [0,1]\) the measurement efficiency of channel \( k\) , and \( \bar{k}\) the number of channels. For \( \eta_k>0\) , measurement signal \( dy_{t,k}\) describes the weak continuous-time equivalent of probabilistic detection results. The randomness is expressed via independent Wiener processes \( dw_{t,k}\) , of mean \( 0\) and variance \( dt\) . The state undergoes a stochastic evolution \( d\rho_t\) correlated with the measurement result, in a weak continuous equivalent of wavefunction collapse, plus effect of interaction with the traveling wave. From the latter, the \( L_k\) need not be Hermitian, and unmonitored channels, \( \eta_k=0\) , model deterministic decoherence.

Itō-type integration means, among others, that nonlinear coordinate changes imply second-order corrections on the differential equation, which do play a role in the results (see Sections 2.1 and 2.2). The equivalent of renormalization at wavefunction collapse makes (1) nonlinear in \( \rho_t\) . By allowing non-normalized states, the nonlinear term in (1) drops. This turns out to only moderately facilitate analysis, so this variant is left aside here.

In [31], studying (1) for a qubit \( \mathcal{H} \simeq \mathbb{C}^2\) , it was found that conditions under which \( \rho_t\) does not diffuse in the whole Bloch sphere but instead remains confined to a deterministically evolving surface or curve for all measurement realizations, match natural experimental settings like [30]. This facilitates computing \( \rho_t\) as a function of the measurement signals \( dy_{t,k}\) , allowing fully explicit formulas to be given both for the actual state and for its predicted distribution over time. The present note extends this program to higher-dimensional quantum systems.

2.1 Algebraic criterion

In general, a single Wiener process combined with non-commuting deterministic dynamics is sufficient to induce diffusion in all dimensions. A classical example is a vertical wheel rolling on a surface, whose orientation changes under noise. Applying a deterministic rolling velocity to the wheel, its position will change randomly; at finite time \( t>0\) , the \( x,y\) position coordinates and the wheel orientation can all take arbitrary independent values, despite having a single noise process. Such “reachability” properties (and more precise variants) are well characterized in control theory, replacing the noise process by a control input [40]. Conversely, model reduction chases cases where this would not be the case, i.e. where knowing the values of some degrees of freedom is sufficient to pin down the values of the others.

Facing (1), it is thus tempting to check, to where the different realizations of \( dw_{t,k}\) can bring the system, by viewing them as control signals and using control theoretic methods. As recalled in appendix of [31], this viewpoint is correct provided the SDE is transformed into Stratonovich form. Indeed, Stratonovich sense SDE’s can be treated like ordinary differential equations regarding coordinate changes. Translation between the two formalisms involves a correction \( d_k\) on the deterministic part, independently for each Wiener process: Itō \( dx_t = f(x_t) \, dt + \sum_{k=1}^{\bar{k}} \, g_k(x)\, dw_{t,k}\) transforms into Stratonovich \( dx_t = \left(f(x_t) + \sum_{k=1}^{\bar{k}} d_k(x_t)\right) \, dt + \sum_{k=1}^{\bar{k}} \, g_k(x)\, \circ\, dw_{t,k}\) with \( d_k = - \frac{1}{2} \sum_{\ell=1}^N \, \frac{\partial g_k}{\partial (x)_\ell} (g_k)_\ell(x)\) , where \( (v)_\ell\) denotes component \( \ell\) of the vector \( v\) . The \( \circ\) in practice is usual multiplication, it just labels Stratonovich sense SDE’s here. For (1), translating the \( g_k,\; d_k\) into \( G_{L_k},\; D_{L_k}\) , the corrective term amounts to

\[ \begin{eqnarray*} D_{L_k}(\rho) &=& -\frac{\eta_k}{2}\Big( L_k G_{L_k}(\rho) + G_{L_k}(\rho) L_k^\dagger \\ \nonumber && ~ ~~ - \text{Tr}\big(L_k G_{L_k}(\rho) + G_{L_k}(\rho) L_k^\dagger \big) \; \rho \\ \nonumber && ~~ ~~ - \text{Tr}\big(L_k \rho + \rho L_k^\dagger\big)\; G_{L_k}(\rho) \Big) \; . \end{eqnarray*} \]

Then the following result holds [41].

Proposition 1

Consider the SDE (1), starting from a given initial state \( \rho_0\) . At any given time \( t\) , the distribution of \( \rho_t\) , over all possible realizations of the measurement process, is confined to a manifold \( \mathcal{M}(t)\) . The dimension \( M\) of \( \mathcal{M}(t)\) equals the dimension of the smallest real Lie algebra \( \mathfrak{G}_F\) generated by the vector fields \( \{ G_{L_k} \}_{k=1}^{\bar k}\) and closed under repeated Lie brackets with the vector field \( -i\, [H, \cdot ] + \sum_{k=1}^{\bar k} \; F_{L_k} + D_{L_k}\) .

The algebraic criterion of Proposition 1 very rapidly checks if a setting may feature low-dimensional \( \mathcal{M}(t)\) ; and therefore, if it seems promising to search for relatively simple explicit expressions of \( \rho_t\) . It has been essential in identifying the situations discussed in Section 3.

2.2 Computing low-dimensional deterministic manifolds in practice

A first point is to compute the commutators of vector fields involved in \( \mathfrak{G}_F\) . This is systematic; the following formulas hold. (Note the two different meanings of the bracket, respectively vector field commutators on the left and operator commutators on the right.)

\[ \begin{eqnarray} \nonumber G_{\alpha I} &\equiv& 0 \text{ for \( I\) the identity and all } \alpha \in \mathbb{C} \\ \nonumber G_{-iH}(\cdot) &\equiv& -i[H,\cdot] \\ [G_{L_j},\,G_{L_k}] & = & G_{[L_j,L_k]} \end{eqnarray} \]

(2)

\[ \begin{eqnarray} [F_{L_j}+\eta_j D_{L_j},\,G_{L_k}](\rho) & = & (1-\eta_j) \, \left([L_j,L_k]\rho L_j^\dagger - \text{Tr}([L_j,L_k]\rho L_j^\dagger)\rho ~ + h.c. \right) \end{eqnarray} \]

(3)

\[ \begin{eqnarray} & & + (1-\eta_j)\, G_{L'}(\rho) + \eta_j \, G_{L''}(\rho) \\ \nonumber & & + \eta_j \big(c_1(\rho)\, G_{[L_j,L_k]}(\rho) + c_2(\rho) G_{L_j}(\rho)\big) \\ \nonumber \text{... with } \;\;\; L' & = & \tfrac{1}{2}\, [L_k,L_j^\dagger L_j] \; , \\ \nonumber L'' & = & \tfrac{1}{2}\, \left[L_k\,,\, (L_j^\dagger+L_j)\, L_j \right] \; , \\ \nonumber \text{special case } j=k : \\ \nonumber [F_{L_j}+\eta_j D_{L_j},\,G_{L_k}] &=& G_{L'} + \eta_j c_2(\rho) G_{L_j} \; ; \\\end{eqnarray} \]

\( h.c.\) denotes hermitian conjugate, while \( c_1(\rho)\) and \( c_2(\rho)\) are real scalar coefficients. The value of these coefficients has no importance since the corresponding vector fields already appear in \( \mathfrak{G}_F\) . For further commutation with vector fields like (3), it can be useful to write it as:

\[ \begin{eqnarray} && [L_j,L_k]\rho L_j^\dagger - \text{Tr}([L_j,L_k]\rho L_j^\dagger)\rho ~ + h.c. \end{eqnarray} \]

(4)

\[ \begin{eqnarray} && = \;\; \left( [L_j,L_k]\rho L_j^\dagger - L_j^\dagger[L_j,L_k] \rho ~ + h.c. \right) + G_{L_j^\dagger [L_j,L_k]}(\rho) \; , \\\end{eqnarray} \]

where the nonlinear part takes the usual form \( G_L\) and the “non-standard” form is linear. A similar procedure can be applied to the vector fields appearing from further commutations. In the present note, the expressions often simplify at an earlier stage.

A second point is to identify the dimension \( M\) spanned by \( \mathfrak{G}_F\) , with some caveats.

  • The map from \( L_k\) to \( G_{L_k}\) is not injective, since for instance \( \{ G_{i \sigma_x}, G_{i \sigma_y}, G_{\sigma_z} \}\) are linearly dependent at any \( \rho\) . Such dependencies can often be identified while searching for the manifold expressions, or by checking numerically at random \( \rho\) .
  • Occasionally, the deterministic dynamics \( \sum_j [F_{L_j}+\eta_j D_{L_j}]\) induces a reduced \( \mathfrak{G}_F\) when the rates of the different channels (magnitudes of \( L_j\) ) take particular values; see e.g. Section 3.3.2. The present note mostly assumes that the rates are not adjusted to such particular values.

A third and last point is the explicit computation of the manifolds. The algebra \( \mathfrak{G}_F\) at each \( \rho\) gives the tangent space to a manifold, among a foliation decomposing the full space of density operators on \( \mathcal{H} \simeq \mathbb{C}^N\) . In principle, this tangent space setting must be integrated to obtain the manifolds themselves. Recall that the manifolds, although independent of the (stochastic) measurement results, do in general evolve (deterministically) with time. Two methods are proposed for computing them more efficiently.

  • By construction, the manifolds are characterized by a vector of \( (N^2-1)-M\) variables, which are nonlinear functions of the components of \( \rho\) , and whose evolution equations are purely deterministic:

    \[ \begin{equation} p_t = h(\rho_t)~ \text{such that} ~ dp_t = f(p_t,t)\, dt \; . \end{equation} \]

    (5)

    Finding these variables is exactly like finding invariants of motion (e.g. surfaces parameterized by the conserved value of energy), except “invariant” is replaced by “deterministically evolving”. Recall the Itō rule to be used when performing changes of variables on (1): For \( x\) of components \( x_j\) and \( dx_j = f_j(x) dt + \sum_k g_{j,k}(x)\, dw_k\) , performing the change of coordinates \( x'_j = h_j(x)\) entails:

    \[ \begin{equation} dx'_j = \sum_l\, \tfrac{\partial h_j}{\partial x_l} f_l dt + \sum_{l,k}\, \tfrac{\partial h_j}{\partial x_l} g_{l,k}\, dw_k + \tfrac{1}{2} \sum_{l,m,k}\, \tfrac{\partial^2 h_j}{\partial x_l \partial x_m} g_{l,k}\, g_{m,k}\, dt \, . \end{equation} \]

    (6)

    The last sum is the Itō correction term. We will thus look for functions \( h(x)\) in which the stochastic part of the evolution drops, and which form a closed dynamical system.

  • A related way to characterize the manifolds is by providing an explicit solution

    \[ \begin{equation} \rho_t = f(\rho_0, r_t, \gamma_t) \; , \end{equation} \]

    (7)

    in which the vector of deterministic parameters \( r_t\) (latin letters) follows a set of ODEs, while the \( M\) -dimensional vector of stochastic parameters \( \gamma_t\) (greek letters) follows measurement-dependent SDEs which cannot be further reduced. Expressions like (7) are more direct to use in filtering applications, but typically only known for specific cases like so-called linear quantum systems [42], where a Gaussian distribution in phase space is preserved. The construction of \( \mathfrak{G}_F\) helps identify all settings where expressions like (7) keep holding and are thus worth seeking after.

2.3 General Remarks

1. The cases \( \eta_j=0\) and \( \eta_j=1\) are special. For \( \eta_j=0\) , the corresponding output \( dy_{t,j}\) gives no information and the SDE governing \( d\rho_t\) treats it as purely deterministic decoherence. When \( \eta_j=1\) for all \( j\) , the quantum measurement recovers maximal information and an initial pure state remains pure for all times. However, this does not mean that the manifolds all remain stationary over time. The interested reader can find counterexamples in the applications below, and e.g. in [31] when measuring \( L_1=\sigma_-\) on a qubit. From a technical viewpoint, when constructing \( \mathfrak{G}_F\) the non-standard term (3) drops out for \( \eta_j=1\) . This special case is not systematically discussed in the applications below.

2. It may be tempting to view the confining manifolds, obtained for \( \eta_j \in (0,1)\) , as a weighted sum of perfect detection case (\( \eta_j=1\) , confinement to pure states) and “no measurement” case (\( \eta_j=0\) ; deterministic evolution), i.e.

\[ \begin{equation} \rho_t = (1-c_t) \, \rho_{\eta=1,t} + c_t \, \rho_{\eta=0,t} \end{equation} \]

(8)

where only the pure state \( \rho_{\eta=1,t}\) would depend on measurement results. As a matter of fact, in general such interpretation fails. For instance:

  • The weighted sum between a pure state and a deterministically evolving point should yield a manifold of dimension \( N-1\) when \( \mathcal{H} \simeq \mathbb{C}^N\) . The case studies observe no such systematic match in dimensions. Already the qubit study in [31] observes: a single generic \( L_1\) , namely all but an obvious variation of either \( L_1= \alpha \sigma_-\) or \( L_1 =\alpha \sigma_z\) with \( \alpha_k \in \mathbb{C}\) , induces diffusion in all directions inside the Bloch sphere.
  • Even for the case where dimensions match, consider for instance \( L=\sigma_z\) measurement on a qubit as in [31]. The eigenstates \( \rho= |g\rangle\langle g|\) and \( \rho= |e\rangle\langle e|\) are part of all \( \mathcal{M}_t\) . To cover the case when e.g. \( \rho_t = |g\rangle\langle g|\) for some \( t\) by chance, we need either \( \rho_{\eta=1,t}=\rho_{\eta=0,t}=|g\rangle\langle g|\) , and thus \( \rho_{\eta=0,t}=|g\rangle\langle g|\) for all \( t\) independently of measurement results; or \( c_t = 0\) for all \( t\) and independently of measurement results. The latter case is obviously vacuous. The former case is obviously incompatible with the possibility to also get \( \rho_t = |e\rangle\langle e|\) .
    Various other properties can be put forward to argue in a similar way.

An interpretation along similar lines may be found in future work, but it thus requires more effort than something simple like (8).

3. Towards computing \( \mathfrak{G}_F\) , the nonlinear part in (1) is not so bothering, as it is a scalar times \( \rho\) . It is often more tedious to just work out the implications of operators piling up on the left and right side of \( \rho\) . The latter feature remains, therefore allowing only moderate simplifications, when considering the linear SDE governing unnormalized \( \rho_t\) . Proposition 1 remains applicable in this case, but it may count a motion direction which is irrelevant when projecting back to normalized density matrices. For \( \mathfrak{G}_F\) computed from the linear unnormalized SDE, one should thus separately check whether it contains the direction corresponding to the trace of \( \rho\) in order to deduce the actual manifold dimension for \( \rho_t\) . We refrain from stating a “generic situation” here, because the whole paper checks out non-generic settings.

3 Case studies

This section summarizes the results of applying the method of Section 2 to several situations which appear relevant in practice. It occasionally discusses physical implications on examples. Section 3.1 considers the case of QND measurements. Section 3.2 considers the measurement of harmonic oscillator quadratures. Section 3.3 considers bipartite quantum systems. Full general formulas for all cases are provided in Appendix, as well as a detailed sketch of their derivation.

3.1 Quantum non-demolition measurement

The QND measurement [4, 43] can be viewed as the weak-measurement equivalent of the Von Neumann projective measurement. Its purpose is to detect the distribution of population on the different eigenstates of a Hermitian operator \( Q=\sum_{n=1}^N q_n |d_n\rangle\langle d_n|\) in the orthonormal basis \( \{|d_n\rangle\}_{n=1}^N\) , without disturbing any eigenstate \( |d_n\rangle\) of \( Q\) . A QND measurement is therefore characterized by channel operators \( L_k\) which commute with \( Q\) . The associated output signals will allow an observer to progressively single out one eigenstate, with associated progressive wavefunction collapse onto that eigenstate. The following results characterize the dynamics of this process according to (1) in more detail.

1.

The theoretical equivalent of projective measurement would assume Hermitian \( L_k\) , thus \( L_k=\sum_{n=1}^N \lambda_k(n) |d_n\rangle\langle d_n|\) with eigenvalues \( \lambda_k(n) \in \mathbb{R}\) . This is called homodyne detection. Note that we do admit \( L_k\) with degenerate eigenvalues here. When \( dy_k\) is the amplitude of an electromagnetic field, with a proper amplification as e.g. in [30], it is natural to measure two field quadratures, corresponding to \( L_k\) and its imaginary multiple \( L_{k'} = i L_k\) . This is called heterodyne dectection.
In both cases, since \( [L_k,L_j] = 0\) and \( [L_k,L_j^\dagger] = 0\) for all \( j,k\) , the system features a confining manifold of dimension \( M \leq \bar{k}\) the number of measurement channels.
When \( \langle d_a| \rho_{t=0} |d_a\rangle=0\) for some \( |d_a\rangle\) , this will remain the case for all \( t>0\) ; this additional reduction eliminates potential singularities in the below expressions.

2.

Denote \( \rho_t(a,b) = \langle d_a| \rho_t |d_b\rangle\) the matrix components in the eigenbasis of the \( L_k\) . For the homodyne case:

Proposition 2

The deterministically evolving manifold is characterized by:

\[ \begin{eqnarray*} \phi^{(a,b)}_t & = & \phi^{(a,b)}_0 \text{ where } \phi^{(a,b)}_t = \mathrm{phase}(\rho_t(a,b)) ~ \text{for all } a,b=1,2,...,N \;\;\;\; ;\\ c^{(a,b)}_t & = & c^{(a,b)}_0 \, e^{\big( - \overline{(1-\eta)(Q(a)-Q(b))^2}\, t \big)} ~ \text{for all } a,b=1,2,...,N \;\;, \\ & & \text{where } \;\;\; c^{(a,b)}_t \; = \; \frac{\vert \rho_t(a,b) \vert^2}{\rho_t(a,a)\rho_t(b,b)} \\ && \text{ and } \;\; \overline{(1-\eta)(Q(a)-Q(b))^2} = {\textstyle \sum_{k=1}^{\bar{k}}} \; (1-\eta_k) (\lambda_k(a)-\lambda_k(b))^2 \;\; ;\\ z^{(\alpha)}_t & = & z^{(\alpha)}_0 \, e^{\big( -2 \sigma^2_\alpha \; t \big)} \\ & & \text{where } z^{(\alpha)}_t = \prod_{b=1}^N \, (\rho_t(b,b))^{\alpha_b} \;\; \text{ and } \;\; \sigma^2_\alpha = \sum_{b=1}^N \sum_{k=1}^{\bar k} \, \alpha_b \, (\lambda_k(b))^2 \, \eta_k \\ & & \text{with any } \alpha\in\mathbb{R}^N \text{ solving } \textstyle \sum_{b=1}^N \alpha_b = 0 \; ,\\ & & \phantom{ \text{with any } \alpha\in\mathbb{R}^N \text{ solving } } \eta_k \; \textstyle \sum_{b=1}^N \alpha_b \, \lambda_k(b) = 0 \;\; \text{for all } k=1,2,...,\bar{k} \, \; ,\\ & & \phantom{ \text{with any } \alpha\in\mathbb{R}^N \text{ solving } } \text{ and } \sigma^2_\alpha \geq 0 \, . \end{eqnarray*} \]

A similar expression can be found in Appendix for the heterodyne case, where the phases \( \phi^{(a,b)}_t\) will also undergo correlated motion. The proof of Proposition 2 is also provided in Appendix.

3.

Let us briefly comment Proposition 2.

The \( c^{(a,b)}_t\) establish how coherences among eigenstates deterministically decay while we are accumulating measurement results. The factor \( (1-\eta_k)\) expresses that for a perfectly efficient measurement \( \eta_k = 1\) , the state remains pure, hence correlations remain at their maximum: the off-diagonals will eventually converge to zero, but only at the same rate as all diagonal elements except a stochastically selected one. On the contrary, for an inefficient measurement \( \eta_k \ll 1\) , the off-diagonals decay faster than the diagonal converges towards a particular measurement eigenvalue. The decay rate reflects how strongly the two eigenstates \( |d_a\rangle,|d_b\rangle\) are distinguished by the QND measurement overall.

While the first two sets of equations essentially generalize [31], the set of equations with \( z^{(\alpha)}_t\) is entirely new. It expresses how the diagonal elements evolve in a correlated way while converging towards one stochastic measurement result. The less measurement channels, the more correlated are the various populations. Since \( z^{(-\alpha)} = 1/z^{(\alpha)}\) and \( \sigma^2_{-\alpha} = -\sigma^2_{\alpha}\) , the inequality constraint just selects variables tending to \( 0\) rather than to \( \infty\) . When \( \eta_k=0\) for some \( k\) , there are more linearly independent choices for \( z^{(\alpha)}\) , yielding a manifold of correspondingly lower dimension. When some levels \( a,b\) are degenerate in all measurement operators, the choice \( \alpha_a=-\alpha_b\) and \( \alpha_c=0\) for all \( c\neq a,b\) expresses the conservation of \( \rho(a,a)/\rho(b,b)\) for these indistinguishable populations. For \( \bar{k} = 1\) , the system is confined to a curve, so knowing \( \rho_0\) and the actual evolution of e.g. \( \rho_t(1,1)\) is sufficient to deduce the evolution of all the other components of \( \rho_t\) !

4.

The form of the \( f^\alpha_t\) can be understood from the following expression of \( \rho_t\) .

Proposition 3

The diagonal components \( \rho_t(b,b)\) in the setting of Proposition 2 have the explicit solution:

\[ \begin{equation} \rho_t(b,b) = \rho_0(b,b) \cdot e^{2 \sum_{k=1}^{\bar k} \;( \lambda_k(b) \sqrt{\eta_k}\, {y^k_t} - \lambda_k(b)^2\eta_k\, t) } \cdot \mu(t) ~ \text{ for all \( b\) ,} \end{equation} \]

(9)

where \( \mu(t)\) is a normalization constant independent of index \( b\) . The values of all the \( \rho_t(b,b)\) at time \( t\) are thus uniquely determined by the \( \bar{k}\) values of the integrated measurement signals \( y^k_t\) up to time \( t\) .

Altogether, this matches the form (7) with \( \gamma_t = (y_{t}^1,...,y_{t}^{\bar{k}})\) stochastic and \( r_t = \{\phi_t^{(a,b)}\,,\;c_t^{(a,b)} \}\) deterministic. The normalization constant \( \mu(t)\) depends on measurement results, but also on \( \rho_0\) since partial wavefunction collapse should make \( \rho_t\) a nonlinear function of \( \rho_0\) while (9) is linear in \( \rho_0\) . This feature will appear at other places when using the form (7); leaving such \( \mu_t\) unspecified is a standard feature of Bayesian filtering, e.g. in robotics too.
In hindsight, all these expressions reflect the property of QND measurements also in discrete time, namely that the order of the measurement results has no impact on the filter state. This indeed justifies the simple integration of the measurement signal in Proposition 3, without any further memory effect.

The above formulas are particularized to a few concrete examples in Appendix. The following summarizes the settings and a few notable observations.

Ex. Quantum number measurement:

This corresponds to the single measurement operator \( L_1 = \mathbf{N} = \sum_{n=0}^{n_{\max}} \, n\, |n\rangle\langle n| \, ,\) as can now be performed routinely in various experimental setups [44, 45, 46]. The most interesting point concerns the correlated evolution of eigenstate populations, where we can obtain various invariant combinations, like:

\[ z_t^{(\alpha)} = \left(\frac{\rho_t(n_4,n_4)}{\rho_t(n_1,n_1)}\right)^{(n_3-n_2)} \left(\frac{\rho_t(n_2,n_2)}{\rho_t(n_3,n_3)}\right)^{(n_4-n_1)} = z_0^{(\alpha)} \; \text{ for any } (n_2-n_1) = (n_4-n_3) \, . \]

Ex. Continuous-variable measurement:

The simplest setting corresponds to \( L_1 = \mathbf{X} = \int_{\mathbb{R}} x\, |x\rangle\langle x| \, dx\) , representing for instance the position operator, in the complete orthonormal basis \( \{|x\rangle\}\) . We also write the density operator \( \rho = \int_{\mathbb{R}^2} \, \rho(x_1,x_2)\, |x_1\rangle\langle x_2| \, dx_1\, dx_2\) in the position representation (accepting a lack of rigor for the uncountably infinite basis). The off-diagonal amplitudes then decay as

\[ c_t(x_1,x_2) = c_0(x_1,x_2) \, e^{-(1-\eta)\, (x_1-x_2)^2 \, t} \; , \]

naturally expressing how coherences between positions further apart decay faster. Regarding the diagonal components, i.e. the population distribution \( p(x) = \rho(x,x)\) along \( x \in \mathbb{R}\) , we obtain in particular:

\[ \begin{eqnarray*} \frac{d^2}{dx^2}[\log p_t(x)] &=& \frac{d^2}{dx^2}[\log p_0(x)] - 2 \eta t \\ \frac{d^k}{dx^k}[\log p_t(x)] &=& \frac{d^k}{dx^k}[\log p_0(x)] \text{ invariant for all } k>2 \, . \end{eqnarray*} \]

Such expressions indicate how most elements of the “shape” of \( p(x)\) are preserved independently of measurement realizations. In the form (7), the continuous limit of (9) becomes:

\[ \begin{eqnarray} p_t(x) &=& p_0(x) \cdot e^{- (x-\gamma_{t})^2/ (2 \sigma_t^2)} \, \cdot \mu_t \\ & & \text{ with } \sigma_t = \frac{1}{\sqrt{2 \eta t}}\;\;\;\; , \;\; \gamma_{t} = \frac{y_t}{\sqrt{\eta} t} \;\;\;\; , \;\; \mu_t \text{ a normalization constant.} \\\end{eqnarray} \]

Thus, we multiply the distribution \( p_0(x)\) by a Gaussian, whose stochastic mean \( \gamma_{t}\) reflects the integrated measurement output, while the standard deviation \( \sigma_t\) decreases deterministically. Finally, we show in appendix how a heterodyne measurement, with \( L_1 = \mathbf{X}\) and \( L_2 = i \, \mathbf{X}\) , induces in addition a particularly correlated evolution of the off-diagonal phases.

Note that here we have assumed no other dynamics than the position measurement \( X\) , which becomes infinitely precise as \( t\) goes to infinity (at the price of infinite uncertainty on momentum, the conjugate variable). In Section 3.2 we add realistic elements to the dynamics, under which the (un)certainties remain finite, and give the corresponding full state expressions in reduced form.

Ex. 3-qubit repetition code

We finish with an example where it is natural to measure several commuting hermitian \( L_k\) , namely in quantum error correction (QEC), see e.g. [25, chapter 10],[47]. In the most common paradigm of stabilizer codes, each \( L_k\) compares adjacent qubits to monitor an error syndrome, with eigenvalues \( \pm 1\) . The eigenspace associated to +1 on all \( L_k\) corresponds to the valid codespace, other measurement results identify corresponding errors.

The simplest error-correcting code is the 3-qubit repetition code. The Hilbert space is \( \mathcal{H}=\text{span}(\{|0\rangle,|1\rangle\} \otimes \{|0\rangle,|1\rangle\} \otimes \{|0\rangle,|1\rangle\}) \simeq \mathbb{C}^8\) and the measurements each compare whether two qubits have the same or a different value in the canonical basis. Denoting \( P_{\{|v_1\rangle,|v_2\rangle,...\}}\) the orthonormal projector onto the subspace spanned by \( v_1,v_2,...\) , we thus have:

\[ \begin{eqnarray*} L_1 &=& P_{\{|0\; 00\rangle,|1\; 00\rangle,|0\; 11\rangle,|1\; 11\rangle \}} - P_{\{|0\; 10\rangle,|1\; 10\rangle,|0\; 01\rangle,|1\; 01\rangle \}} \\ L_2 &=& P_{\{|0\, 0 \, 0\rangle,|0\, 1\, 0\rangle,|1\, 0\, 1\rangle,|1\, 1 \, 1\rangle \}} - P_{\{|1\, 0\, 0\rangle,|1\,1\, 0\rangle,|0\, 0 \, 1\rangle,|0 \, 1\, 1\rangle \}} \\ L_3 &=& P_{\{|00 \; 0\rangle,|00 \; 1\rangle,|11 \; 0\rangle,|11 \; 1\rangle \}} - P_{\{|10 \; 0\rangle,|10 \; 1\rangle,|01 \; 0\rangle,|01 \; 1\rangle \}} \; . \end{eqnarray*} \]

Together, these \( L_k\) distinguish four eigenspaces, each one twofold degenerate:

\[ \begin{align*} (\lambda_1(.),\lambda_2(.),\lambda_3(.)) &\; =(+1,+1,+1) & \text{ on } \text{span}(|000\rangle,|111\rangle)=:V_0 \; ; \\ & \; =(+1,-1,-1) & \text{ on } \text{span}(|100\rangle,|011\rangle)=:V_1 \; ; \\ &\; =(-1,+1,-1) & \text{ on } \text{span}(|010\rangle,|101\rangle)=:V_2 \; ; \\ & \; =(-1,-1,+1) & \text{ on } \text{span}(|001\rangle,|110\rangle)=:V_3 \; . \end{align*} \]

The twofold degeneracy gives the possibility to encode a qubit in the codespace \( |\psi\rangle = c_0 |000\rangle + c_1 |111\rangle\) ; in the other eigenspaces, it allows to identify a single spurious bit-flip \( 0 \leftrightarrow 1\) , via changes in the measured eigenvalues, without any loss of quantum information \( c_0,c_1\) .

  • In the form of Proposition 2, we have \( c^{(a,b)}_t = c^{(a,b)}_0\) when \( (|a\rangle,|b\rangle) \subset V_k\) for some \( k\) (no loss of encoded quantum information) and \( c^{(a,b)}_t = c^{(a,b)}_0 \, e^{-(1-\eta) 8 t}\) otherwise (two of the three syndromes \( L_k\) differentiate \( V_j\) from \( V_{j'\neq j}\) , inducing decay of coherences among them). Regarding diagonal elements, \( z^{(\alpha)}_t = \frac{\rho_t(a,a)}{\rho_t(b,b)} = z^{(\alpha)}_0\) is conserved for \( (|a\rangle,|b\rangle) \subset V_k\) for each \( k=0,1,2,3\) . This just says that within each eigenspace, relative populations do not change. Since we expect stochastic motion along \( 3\) dimensions, there are no further deterministic correlations among diagonal elements: the relative populations between the different eigenspaces \( V_0,\, V_1,\, V_2,\, V_3\) can evolve in all directions as a function of the three measurement signals. In the form of Proposition 3, we can thus write in particular \( \; \rho_t(a,b) = \rho_0(a,b) \gamma_{t,k} \;\) for each \( 2\times2\) matrix block corresponding to a subspace \( (|a\rangle,|b\rangle) \subset V_k\) , with the real numbers \( \gamma_{t,k}\) evolving independently (up to overall normalization) as a function of measurement results. The evolution of the other \( 2\times2\) matrix blocks, corresponding to a coherence between two different subspaces \( V_k,V_j\) , is then deduced from the evolution of these diagonals and the deterministic dynamics of \( c^{(a,b)}_t\) .
  • In the above setting, one measurement channel is redundant: applying only e.g. \( L_1\) and \( L_3\) measurements is sufficient towards identifying to which subspace \( V_k\) the state belongs. Then \( \mathcal{M}_t\) has one dimension less and there is another deterministic variable. Solving for \( \alpha\) according to Proposition 2 yields:

    \[ z^{(\alpha*)}_t = \frac{\rho_t(000,000) \rho_t(010,010)}{\rho_t(001,001)\rho_t(100,100)} = z^{(\alpha*)}_0 \; . \]

    The conservation of \( z^{(\alpha*)}\) indicates how, when e.g. the state converges towards \( V_0\) under stochastic measurement results, the population on \( V_2\) must converge to zero quicker than the populations on \( V_1\) and \( V_3\) . This reflects that confusing \( V_0\) with \( V_2\) would correspond to confusing the eigenvalues of both \( L_1\) and \( L_3\) , whereas confusing e.g. \( V_0\) and \( V_1\) implies confusion on a single measurement operator. The \( c^{(a,b)}_t\) similarly follow different decay rates in absence of \( L_2\) .

  • The repetition code is meant to counter spurious bit flips. These are added to the model through operators \( L_{3+k}=\sqrt{\Gamma_k} \sigma_{x,k}\) , where \( \sigma_{x,k} = |0\rangle\langle 1|+|1\rangle\langle 0|\) on qubit \( k\) , and with \( \eta_4=\eta_5=\eta_6=0\) . Thus the SDE is driven by no new stochastic processes. However, as in the classical example with the rolling wheel, the commutation of stochastic vector fields with new deterministic dynamics can induce diffusion in many more directions. This turns out to be the case here indeed, as we have quickly generated up to 15 different vector fields in \( \mathfrak{G}_F\) by hand even for the special situation \( \eta_1=\eta_2=\eta_3\) and \( \Gamma_1=\Gamma_2=\Gamma_3\) (see appendix). There is thus no drastic and exact model reduction in this realistic situation, compared to modeling the full state \( \rho_t\) with 64-1 real components. In other words: the 3 values of integrated measurement results \( y_{t,1}, y_{t,2}, y_{t,3}\) would not be enough anymore to identify the state, and in fact the associated memory effect would have to be modeled with at least 15 variables. An idea towards efficient approximate model reduction, requiring little online adaptation [27], could be to typically drop terms corresponding to higher-order commutators. Anyways, any small approximate continuous-time model may already help refine error-correction decisions compared to a discrete-time projective measurement model.

3.2 Measuring harmonic oscillator quadratures

The quantum harmonic oscillator is a paradigmatic model of quantum physics [4]. Its infinite-dimensional Hilbert space is the \( L_2\) functions. The eigenvalues of the bare system Hamiltonian \( H_0\) are evenly spaced and transitions are governed by the annihilation operator \( \bf{ a}\) and creation operator \( \bf{ a}^†\) , which follow the fundamental commutation property \( [\bf{ a},\bf{ a}^\dagger] = \bf{ I}\) the identity, and play a prominent role in its processes. In particular, \( H_0\) is proportional to \( \bf{ a}^† \bf{ a}\) . The two quadratures \( \bf{ X} = \tfrac\bf{{ a}+\bf{ a}^\dagger}{2}\) and \( \bf{ P} = \tfrac\bf{{ a}-\bf{ a}^\dagger}{2i}\) , corresponding to the position and momentum operators in a mechanical embodiment, are typical interaction operators appearing in measurements and as control Hamiltonians.

Several typical experimental measurement settings on this system have no projective equivalent. They nevertheless feature confining deterministic manifolds \( \mathcal{M}_t\) , which the following characterizes in the form (7) on the Wigner function \( \mathcal{W}^{\{\rho\}}(x,p)\) . The latter can be seen as a quasi-probability distribution in \( \bf{ X},\bf{ P}\) phase space (see appendix). The Gaussian kernels obtained below in \( \mathcal{W}^{\{\rho\}}(x,p)\) can be viewed as a generalization of the preservation of Gaussian states by both forward and backward quantum filters [48]. In the Heisenberg picture, those examples can be approached as so-called linear quantum systems [42].

3.2.1 Monitoring the annihilation channel

Also known as fluorescence measurement [49, 50, 51], this setting corresponds to using \( L_1=\bf{ a}\) and possibly \( L_2=i\bf{ a}\) in a heterodyne detection. The corresponding outputs

\[ \begin{eqnarray*} dy_{t,1} &=& 2\sqrt{\eta_1} \text{Trace}({\bf X} \rho_t)\, dt + dw_{t,1} ~ , \\ dy_{t,2} &=& -2\sqrt{\eta_2} \text{Trace}({\bf P} \rho_t)\, dt + dw_{t,2} \; \end{eqnarray*} \]

inform about position and momentum, but unlike e.g. with \( L_1=\bf{ X}\) , the system actually emits energy and progressively decays towards its ground state \( |0\rangle\) . This is strictly analogous to \( L_1=\sigma_-\) and \( L_2 = i \sigma_-\) on a qubit, as in [30] whose experimental data has motivated the present work. The following facts are obtained in detail in Appendix.

1.

According to Proposition 1, just measuring \( L_1\) and \( L_2\) in presence of \( H_0 = \Delta \bf{ a}^\dagger \bf{ a}\) yields deterministic manifolds of dimension 2. Adding a Hamiltonian proportional to any combination of \( \bf{ X}\) and \( \bf{ P}\) , which is the form of typical control signals, does not change the manifold dimension. When the system decays into an environment of nonzero temperature \( n_{th} > 0\) , an operator \( L_3=\bf{ a}^†\) is added with \( \eta_3=0\) . This situation features deterministic manifolds of dimension 4. When \( \Delta=0\) and not measuring \( L_2\) (homodyne detection), all these dimensions are divided by two.
Thus, for \( n_{th} >0\) , attempting to describe the state with a smart integral of each output signal is bound to fail. Nevertheless, it is sufficient to track two integrals per output channel, in order to capture the corresponding memory effect, and obtain again a compact and fully general description of \( \rho_t\) .

2.

The aim is thus to write the solution in compact form for the SDE:

\[ \begin{eqnarray} d\rho_t &=& -i\, [u_t ({\bf a}+{\bf a}^†) - iv_t ({\bf a}-{\bf a}^†) \, , \; \rho_t ] \, dt \end{eqnarray} \]

(10)

\[ \begin{eqnarray} && + 2\, (1+n_{th})\, ({\bf a} \rho_t {\bf a}^† - \tfrac{1}{2} {\bf a}^† {\bf a} \rho_t - \tfrac{1}{2} \rho_t {\bf a}^† {\bf a})\, dt\\ \nonumber && + 2\, n_{th} ({\bf a}^† \rho_t {\bf a} - \tfrac{1}{2}{\bf a}{\bf a}^†\, \rho_t - \tfrac{1}{2}\rho_t \, {\bf a}{\bf a}^† ) \, dt \\ \nonumber && + \sqrt{\eta}({\bf a} \rho_t + \rho_t {\bf a}^† - \text{Tr}({\bf a}\rho_t + \rho_t {\bf a}^†)\rho_t )\, dw_{t,1} \\ \nonumber && + i\sqrt{\eta}({\bf a} \rho_t - \rho_t {\bf a}^† - \text{Tr}({\bf a}\rho_t - \rho_t {\bf a}^†)\rho_t )\, dw_{t,2} \; . \\\end{eqnarray} \]

Here \( u_t\) and \( v_t\) are real control signals, possibly time-dependent, and \( \Delta=0\) without loss of generality by redefining variables in a rotating frame. Inspired by the Gaussian form observed in the QND measurement of \( \bf{ X}\) , the following result is obtained.

Proposition 4

The solution of the SDE (10) writes in Wigner representation:

\[ \mathcal{W}^{ \{\rho\} }_t(x,p) = \int \int \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\, K_{x,t}(x,x_0)\, K_{p,t}(p,p_0) \, dx_0\, dp_0\; \nu_t \]

where \( \nu_t\) is a normalization constant and

\[ \begin{eqnarray*} K_{x,t}(x,x_0) &=& \exp\left( \frac{-(x-x_0 a_t - \xi_t)^2}{s_t} + (d_t \, x_0^2+\theta_{t}x_0) \right)\;\; , \\ K_{p,t}(p,p_0) &=& \exp\left( \frac{-(p-p_0 a_t - \pi_t)^2}{s_t} + (d_t \, p_0^2+\phi_{t}p_0) \right)\;\;. \end{eqnarray*} \]

The variables \( a_t, s_t, d_t\) evolve deterministically, i.e. independently of measurement realizations \( dw_{t,1},dw_{t,2}\) , and independently of the control signals. The system of 4 variables \( \xi_t, \pi_t, \theta_t, \phi_t\) depends on controls, and for \( n_{th}>0\) it diffuses stochastically in all dimensions as a function of \( dw_{t,1},dw_{t,2}\) . For \( n_{th}=0\) , variable \( \theta_t\) (resp. \( \phi_t\) ) is related to \( \xi_t\) (resp. \( \pi_t\) ) via a deterministic relation.

The solutions for the evolution of those variables, as well as the full proof, can be found in appendix.

3.

This result concerns the most general initial condition. It may further simplify for particular \( \rho_0\) . For instance, for \( n_{th}=0\) and starting with a so-called coherent state \( \rho_0 = |\alpha\rangle\langle \alpha|\) , \( \alpha \in \mathbb{C}\) , the solution \( \rho_t\) is independent of measurement results. Indeed, the Lindblad equation which reflects the mixture over all possible measurement realizations then remains in a pure state \( \rho_t = |\alpha(t)\rangle\langle \alpha(t)|\) , and this is only possible if all measurement-conditioned trajectories coincide [52, Ch.4,Lem.2].

3.2.2 Measuring position and momentum simultaneously

Taking \( L_1=\bf{ X} = \frac\bf{{ a}+\bf{ a}^†}{2}\) and \( L_2 = \bf{ P} = \frac\bf{{ a}-\bf{ a}^†}{2i}\) yields the same output channels as in Section 3.2.1, but with a very different backaction on \( \rho_t\) . Indeed, the latter is closer to a QND behavior where the mean values of \( \bf{ X}\) and \( \bf{ P}\) do not move on average.

1.

Despite \( \bf{ X}\) and \( \bf{ P}\) not commuting, \( [G_\bf{ X},\, G_\bf{ P}] = 0\) . In the criterion of Proposition 1, commutation with the deterministic dynamics gives two new vector fields \( G_{i\bf X},\, G_{i\bf P} \in \mathfrak{G}_F\) . Further commutations give no new element. Adding Hamiltonians in \( \bf{ X}\) , \( \bf{ P}\) , \( \bf{ a}^† \bf{ a}\) and dissipation in a thermal environment (\( L_3=\sqrt{(1+n_{th})}\bf{ a}\) , \( L_4=\sqrt{n_{th}}\bf{ a}^†\) with \( \eta_3=\eta_4=0\) ) maintains this property. In all cases, there are thus deterministic manifolds of dimension 4.

2.

A most general setting introduces different rates on the two channels. Then, defining \( \tilde\bf{ X}_t = \cos(\Delta t)\, \bf{ X} + \sin(\Delta t)\, \bf{ P}\) and \( \tilde\bf{ P}_t = \cos(\Delta t)\, \bf{ P} - \sin(\Delta t)\, \bf{ X}\) in a rotating frame with respect to \( H_0 = \Delta \bf{ a}^\dagger \bf{ a}\) , we consider the model:

\[ \begin{eqnarray} d\rho_t &=& -i\, [u_t ({\bf a}+{\bf a}^†) - iv_t ({\bf a}-{\bf a}^†) \, , \; \rho_t ] \, dt \end{eqnarray} \]

(11)

\[ \begin{eqnarray} && + \Gamma_\ell\, (1+n_{th})\, ({\bf a} \rho_t {\bf a}^† - \tfrac{1}{2} {\bf N} \rho_t - \tfrac{1}{2} \rho_t {\bf N})\, dt\\ \nonumber && + \Gamma_\ell\, n_{th} ({\bf a}^† \rho_t {\bf a} - \tfrac{1}{2} ({\bf N+I})\rho_t - \tfrac{1}{2}\rho_t({\bf N+I})) \, dt \\ \nonumber && + \Gamma_x (\tilde{\bf X}_t \rho_t \tilde{\bf X}_t - \tfrac{1}{2} (\tilde{\bf X}_t)^2\, \rho_t - \tfrac{1}{2}\rho_t\, (\tilde{\bf X}_t)^2) \, dt \\ \nonumber && + \Gamma_p (\tilde{\bf P}_t \rho_t \tilde{\bf P}_t - \tfrac{1}{2} (\tilde{\bf P}_t)^2\, \rho_t - \tfrac{1}{2}\rho_t\, (\tilde{\bf P}_t)^2) \, dt \\ \nonumber && + \sqrt{\Gamma_x \eta_x}(\tilde{\bf X}_t \rho_t + \rho_t \tilde{\bf X}_t - \text{Tr}(2 \tilde{\bf X}_t\rho_t )\rho_t )\, dw_{t,1} \\ \nonumber && + \sqrt{\Gamma_p \eta_p}(\tilde{\bf P}_t \rho_t - \rho_t \tilde{\bf P}_t - \text{Tr}(2 \tilde{\bf P}_t\rho_t )\rho_t )\, dw_{t,2} \; . \\\end{eqnarray} \]

Proposition 5

The solution of the SDE (11) writes in Wigner representation:

\[ \mathcal{W}^{\{\rho\}}_t(x,p) = \int \int \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\, K_{t}(x,x_0,p,p_0)\, dx_0\, dp_0\; \nu_t \]

where \( \nu_t\) is a normalization constant and

\[ \begin{eqnarray*} K_{t}(x,x_0,p,p_0) &=& \exp\big[ -(q-A_t x_0 - R_t p_0 - \Theta_t)^T (S_t)^{-1} (q-A_t x_0 - R_t p_0 - \Theta_t)\\ && ~ ~~ + (q_0)^T F_t q_0 + (\Lambda_t)^T (\, A_t x_0 + R_t p_0 \,) \big]\; , \end{eqnarray*} \]

with column vectors \( q = (x \,; \; p) \in \mathbb{R}^2\) and \( q_0 = (x_0 \,; \; p_0) \in \mathbb{R}^2\) . The symmetric matrices \( S_t, F_t \in \mathbb{R}^{2\times 2}\) and the vectors \( A_t, R_t \in \mathbb{R}^2\) follow deterministic ODEs, independent of measurement realizations \( dw_{t,1}, dw_{t,2}\) . The vectors \( \Theta_t\) and \( \Lambda_t\) \( \in \mathbb{R}^2\) follow a system of SDEs, diffusing as a function of \( dw_{t,1}, dw_{t,2}\) .

The block-triangular set of equations governing these variables is provided in appendix, with simplifications in special cases. The proof is also given in appendix.

3.

Putting \( \Gamma_p=0\) yields back a QND measurement of \( L_1=\bf{ X}\) (see Section 3.1), now associated to further dynamics. For a general \( \Delta\) and thermal environment, \( \rho_t\) then remains confined onto \( \mathcal{M}_t\) still of dimension 4, and best described by Proposition 5 ; when \( \Delta=0\) , it reduces to dimension 2; when in addition \( \Gamma_{\ell}=0\) , it reduces to dimension 1 in agreement with Proposition 2.

3.3 Bipartite quantum systems

Identifying low-dimensional manifolds is particularly valuable when facing multi-partite quantum systems, whose dimension grow as the product of its components. While the general method remains applicable, this section focuses on particular examples which exploit the bipartite structure.

3.3.1 Indirect Measurement

Consider a system on a bipartite Hilbert space \( \mathcal{H} = \mathcal{H}_A \otimes \mathcal{H}_B\) , where subsystem A is coupled to subsystem B through a Hamiltonian, while only subsystem B is measured. Thus:

\[ \begin{eqnarray} d\rho &=& \left(\, -i\left[\,H_A \otimes {\bf I} + {\bf I} \otimes H_B + {\textstyle \sum_{m=1}^{\bar{m}}} A_m \otimes B_m \, ,\; \rho\,\right] \, \right) \; dt \end{eqnarray} \]

(12)

\[ \begin{eqnarray} && + \left( \sum_{\ell=1}^{\bar{\ell}} F_{M_\ell \otimes {\bf I}}(\rho) \, \right) \; dt + \left( \sum_{k=1}^{\bar{k}} F_{{\bf I} \otimes L_k}(\rho)\, \right) \; dt \\ \nonumber && + \sum_{k=1}^{\bar{k}} \,\sqrt{\eta_k} G_{{\bf I} \otimes L_k}(\rho) \; dw_{t,k}\; . \\\end{eqnarray} \]

This setting, where A is indirectly measured through B, appears in many quantum experiments, see e.g. [44, 46, 45] and many more.

  1. Investigating the algebraic criterion from Proposition 1 quickly shows that the bipartite structure (12) does not imply, on its own, low-dimensional deterministic confining manifolds. Indeed, after characterizing the manifold algebra \( \mathfrak{G}_B\) for subsystem B alone assuming \( B_m = 0\) \( \forall m\) , there remains to check how the coupling Hamiltonian modifies the commutation of \( \mathfrak{G}_B\) with the deterministic dynamics.
    Recalling that \( [A_1\otimes B_1\,,\, A_2\otimes B_2 ] = A_1 A_2 \otimes [B_1\,,\,B_2] + [A_1\,,\,A_2] \otimes B_2 B_1\) , a first commutation of \( A_m \otimes B_m\) with \( L=I \otimes B_k\) for some \( G_L \in \mathfrak{G}_B\) yields an operator of the type \( A_m \otimes B_{k,m}\) . Even assuming \( [A_k,A_j]=0\) \( \forall k,j\) , a next commutation with some \( A_n \otimes B_n\) would yield \( A_n A_m \otimes B_{k,m,n}\) ; thus while the operators on \( \mathcal{H}_B\) may keep cycling within a small algebra, powers of the \( A_k\) accumulate in front, as long as \( B_{k,m,n \neq 0}\) . This indicates that in general, the setting produces diffusion in many if not all directions of \( \mathcal{H}_A \otimes \mathcal{H}_B\) .
  2. In particular, the above structure is often used with \( \eta=0\) to engineer an effective quantum dissipation on system A, stabilizing it into some target set of states [53, 54]. In this case, it is possible to write a reduced model, governing essentially only the dynamics of system A while taking the effects induced by B into account. Such model reduction can be performed with so-called adiabatic elimination [55, 56], which singles out an invariant eigenspace of the Lindbladian evolution and can thus in principle be exact [57] for any system. Point 1. implies that such exact model reduction is not a general property at \( \eta\neq0\) , since often, each state of the joint state space can be moved in all directions by the backaction of the measurements.
  3. Several particular cases do feature interesting manifolds.
    If all the coupling terms commute with the B dynamics, i.e. \( \; [B_m\, , \, L] = 0   \text{for all } m\in\{1,2,...,\bar{m}\} \text{ and all } G_L \in \mathfrak{G}_B \; \) , then \( \mathfrak{G}_F = \mathfrak{G}_B\) . This holds for instance when the \( B_m\) are diagonal in the basis of a QND measurement on \( \mathcal{H}_B\) . Notably, this allows any dynamics on subsystem A, which can imply complicated motion of the joint system, but does not affect the diffusion implied by measurement backaction.
    The following examples are other typical experimental scenarios in which deterministic manifold structures appear.

3.3.1.1 Ex. monitored harmonic oscillator, dispersively coupled to a qudit:

Consider subsystem B a harmonic oscillator (photon annihilation operator \( \bf{ b}\) ) and subsystem A a finite-dimensional system on \( \mathcal{H}_A \simeq \mathbb{C}^d\) , with the dynamics:

\[ \begin{eqnarray} d\rho_t &=& \left(\, -i[\chi Q_A \otimes ({\bf b}^† {\bf b}),\, \rho_t ] -i[{\bf I} \otimes (u_t ({\bf b}+{\bf b}^\dagger) - iv_t ({\bf b}-{\bf b}^\dagger))\,,\, \rho_t \,]\; + 2F_{{\bf I} \otimes {\bf b}}(\rho_t) \, \right) dt \;\; \end{eqnarray} \]

(13)

\[ \begin{eqnarray} && + \sqrt{\eta}\, G_{{\bf I} \otimes {\bf b}}(\rho_t)\, dw_{t,1} + \sqrt{\eta}\, G_{{\bf I} \otimes i{\bf b}}(\rho_t)\, dw_{t,2} \; . \\\end{eqnarray} \]

Operator \( Q_A\) is Hermitian and no other dynamics are allowed on subsystem A, while \( u_t+i v_t\) is a control signal on subsystem B whose annihilation channel is monitored. This setting is typical in “dispersive readout” of qubits with \( Q_A=\sigma_z\) , see e.g. [58, 59]. It can be viewed as an indirect QND measurement of \( Q_A = \sum_{s=1}^d \, \lambda_s \, |s\rangle\langle s|\) , considered non-degenerate here for simplicity of notation. Previous work has established compact expressions for solutions of (13) for particular initial conditions, e.g. a separable initial state with subsystem B in a coherent state [59]. The following provides a low-dimensional characterization of the solution for any initial state — see proof in Appendix.

  • For \( u_t=v_t=0\) , the manifolds \( \mathcal{M}_t\) are of dimension \( 2d\) and characterized by the Abelian algebra: \( \; \mathfrak{G}_F = \text{span}\{G_{|s\rangle\langle s| \otimes \delta \bf{ b}} : s=1,2,...,d;\; \delta =1,i \} \; .\) For general control signals, \( \mathcal{M}_t\) has dimension \( 4d-2\) , characterized by the Abelian algebra: \( \; \mathfrak{G}_F = \text{span}\{G_{|s\rangle\langle s| \otimes \delta \bf{ b}} : s=1,2,...,d;\; \delta =1,i \} \cup \{ G_{|s\rangle\langle s| \otimes \delta \bf{ I}} : s=1,2,...,d-1;\; \delta =1,i \} \; .\) Furthermore, the set of states reachable by system (13), under all measurement realizations and all control signals \( u_t,v_t\) , is confined to a time-dependent manifold \( \tilde{\mathcal{M}}_t\) of dimension \( 3 d^2 +2d - 1\) . This provides the minimal representation linking input and output signals of (13).

    The presence of drives on the harmonic oscillator here modifies the manifold dimension, unlike when the harmonic oscillator was considered alone. More detrimental modifications — in the sense of increasing the manifold dimension — seem to show up when trying to add thermal photons, or when adding dynamics on subsystem A which does not commute with \( Q_A\) . From a complementary viewpoint, this bounds the controllability of the qudit-harmonic oscillator joint system [60], when seeing measurement-induced evolution as a resource; and thus in principle, including any devisable feedback control protocols.

  • The full solution can be expressed in the form \( \rho_t = \sum_{j,k=1}^{d} |j\rangle\langle k| \otimes \rho_{t,(j,k)} \; ,\) where each \( \rho_{t,(j,k)}\) follows a Gaussian kernel, see Appendix. For \( u_t=v_t=0\) , all the variables are deterministically tied to the Gaussian means of diagonal elements \( \rho_{t,(k,k)}\) . Nonzero control signals further induce stochastic components in the relative normalizations of these Gaussians. The algebraic criterion has been an invaluable tool in initiating (and stopping) the search for dependencies among the variables involved.
  • Asymptotically, for large times, the full solution characterizes the following behavior:
    The harmonic oscillator state \( \rho_{t,(k,k)}\) converges towards a so-called coherent state \( =|\alpha_k\rangle\langle \alpha_k|\) whose amplitude \( \alpha_k\) is conditioned on qudit level \( k\) , possibly moving under control drives, but independent of the measurement results.
    For \( \eta \ll 1\) (or if the system is initialized with the \( |\alpha_k\rangle\langle \alpha_k|\) ), the qudit level populations still undergo significant dynamics after this initial transient; these dynamics correspond to the standard QND measurement process, with \( k\) -conditioned coherent state amplitudes \( \alpha_k\) replacing the measurement eigenvalues of Section 3.1. See Appendix for details.

3.3.1.2 Ex. two resonantly coupled harmonic oscillators:

Consider subsystem B a harmonic oscillator (photon annihilation operator \( \bf{ b}\) ) and subsystem A another harmonic oscillator (photon annihilation operator \( \bf{ a}\) ), with the dynamics:

\[ \begin{eqnarray} d\rho &=& \left(\, -i g\, [ {\bf a} \otimes {\bf b}^† + {\bf a}^† \otimes {\bf b}\,,\; \rho\, ] -i[ (\Delta {\bf a}^† {\bf a} + u_t ({\bf a}+{\bf a}^\dagger) - iv_t ({\bf a}-{\bf a}^\dagger) ) \otimes {\bf I}\,,\; \rho \,]\; \right) dt \end{eqnarray} \]

(14)

\[ \begin{eqnarray} &&+ 2(1+n_{th})F_{{\bf I} \otimes {\bf b}}(\rho)\, dt + 2n_{th} F_{{\bf I} \otimes {\bf b}^†}(\rho)\, dt + \sqrt{\eta}\, G_{{\bf I} \otimes {\bf b}}(\rho)\, dw_{t,1} + \sqrt{\eta}\, G_{{\bf I} \otimes i{\bf b}}(\rho)\, dw_{t,2} \; . \\\end{eqnarray} \]

Such coupling model is obtained after Rotating Wave Approximation in a dipolar coupling between quasi-resonant oscillators A and B, with \( u_t+i v_t\) a complex drive amplitude on A and \( \Delta\) expressing a small residual resonance mismatch [4, Chap.3.2]. When the B subsystem is subject to heterodyne measurement and a thermal environment, this is again a linear quantum system [42].

  • The system (14) with \( n_{th}>0\) features deterministic manifolds \( \mathcal{M}_t\) of dimension \( 8\) , characterized by the algebra:

    \[ \mathfrak{G}_F = \text{span}\{G_{\delta {\bf b}},\, G_{\delta {\bf b}^†},\, G_{\delta {\bf a}},\, G_{\delta {\bf a}^†};\; \delta =1,i \} \; . \]

    For \( n_{th}=0\) , the manifold further reduces to dimension 4 as all the \( ^†\) terms in \( \mathfrak{G}_F\) disappear.

    Proof: Operators acting on B alone generate an algebra: \( \mathfrak{G}_B = \text{span}\{\, G_\bf{ b}\,,\; G_{i\bf{ b}} \, \} \; \) when \( n_{th}=0\) , adding \( G_\bf{{ b}^†},\; G_{i\bf{ b}^†}\) for \( n_{th}>0\) . The commutator of \( G_\bf{ b}\) (respectively \( G_\bf{{ b}^†}\) ) with the coupling Hamiltonian just yields \( G_\bf{ a}\) (respectively \( G_\bf{{ a}^†}\) ). Commutation of the latter two yields \( G_{[\bf{ a},\bf{ a}^†]} = G_\bf{ I} = 0\) . Further commutation of these A-dynamics with any B-dynamics vanishes. Further commutation of these A-dynamics with the coupling Hamiltonian yields back \( G_\bf{ b}\) and \( G_\bf{{ b}^†}\) . Hence the algebra is closed at this point. \( \square\)

  • Adding simple dynamics on the B subsystem would not change this manifold structure. First, detuning on B, i.e. a Hamiltonian term in \( \bf{ I} \otimes \tilde\Delta \bf{ b}^† \bf{ b}\) , would be symmetric to detuning on A, by going to another rotating frame; this does not change the dissipation on B, it just implies re-combining the output ports \( dy_{t,1}\) and \( dy_{t,2}\) accordingly with the quadratures’ new rotation speed, and similarly for the control signals on A. Second, adding drives on B, i.e. a Hamiltonian term in \( \bf{ I} \otimes (\tilde{u}_t (\bf{ b}+\bf{ b}^\dagger) - i\tilde{v}_t (\bf{ b}-\bf{ b}^\dagger) )\) , can also be converted into drives on the A subsystem. Indeed, notice that

    \[ g ({\bf a} \otimes {\bf b}^† + {\bf a}^† \otimes {\bf b}) + {\bf I} \otimes (\tilde{u}_t ({\bf b}+{\bf b}^\dagger) - i\tilde{v}_t ({\bf b}-{\bf b}^\dagger) ) = g (({\bf a}+\beta_t) \otimes {\bf b}^† + ({\bf a}+\beta_t)^† \otimes {\bf b})\; , \]

    with \( \beta_t = \frac{\tilde{u}_t + i \tilde{v}_t}{g}\) . Hence, consider the time-dependent unitary change of frame \( \tilde{\rho}_t = \bf{ U}_t \rho_t \bf{ U}_t^\dagger\) with \( \bf{ U}_t = \bf{ D}(\beta_t) \otimes \bf{ I}\) . Here \( \bf{ D}(\alpha) = \exp(\alpha \bf{ a}^† - \alpha^* \bf{ a})\) is the displacement operator [4] on harmonic oscillator mode A, satisfying \( \bf{ D}(\alpha)\, \bf{ a}\, \bf{ D}(\alpha)^\dagger = \bf{ a} - \alpha\) and \( \tfrac{d\bf{ D}(\alpha_t) }{dt}\, \bf{ D}(\alpha_t)^\dagger = \tfrac{d\alpha}{dt} \bf{ a}^\dagger - \tfrac{d\alpha^*}{dt} \bf{ a} + (\tfrac{d\alpha}{dt}\alpha^* - \tfrac{d\alpha^*}{dt} \alpha)\, \bf{ I}\) . With these elements and since \( \bf{ U}_t\) commutes with subsystem B, one checks that \( d\tilde{\rho}\) follows the same equation (14), except \( u_t\) and \( v_t\) are replaced by \( u_t - \tfrac{\Delta \tilde{u}_t}{g} + \tfrac{d\alpha^*/dt-d\alpha/dt}{2i}\) and \( v_t - \tfrac{\Delta \tilde{v}_t}{g} + \tfrac{d\alpha^*/dt+d\alpha/dt}{2}\) respectively.

  • This structure is not surprising, since (14) again models a so-called linear quantum system [42], now on two harmonic oscillator modes. The state can again be expressed with a Gaussian kernel, on the Wigner function in joint state space. We leave the derivation of the corresponding expression as an exercise, possibly exploiting linear quantum systems theory which has notably contributed to the study of such networks of modes.

3.3.2 Indistinguishable emission

Detecting photons emitted by several quantum systems without distinguishing which one has emitted them is a standard experiment, for instance to generate entanglement among two qubits [61, 62, 63].

We here consider a diffusive version of this setting, motivated mainly by the tools developed in Section 2, but also by the fact that field quadrature measurements are experimentally more developed than photodetection for instance in superconducting circuit platforms [64, 65]. The system involves two qubits A and B and is governed by the SDE :

\[ \begin{eqnarray} d\rho_t &=& F_{L_1}(\rho_t)\, dt + F_{L_2}(\rho_t)\, dt + G_{L_1}(\rho_t) \, \sqrt{\eta_1} \, dw_{t,1} + G_{L_2}(\rho_t) \, \sqrt{\eta_2} \, dw_{t,2} \end{eqnarray} \]

(15)

\[ \begin{eqnarray} && \text{ with } L_1 = (\sigma_{-A} + \sigma_{-B})/\sqrt{2} ~ \text{ and } ~ L_2 = i (\sigma_{-A} - \sigma_{-B})/\sqrt{2} \; , \\\end{eqnarray} \]

where \( \sigma_{-k}\) is the jump operator from excited to ground state on qubit \( k\) . Channel operators \( L_1\) and \( L_2\) are obtained in practice, from signals coming from the two individual qubits, after interfering them on a balanced beamsplitter [63]. This justifies why \( L_1\) and \( L_2\) have the same measurement rate .

  • Regarding the algebraic criterion, \( G_{L_1}\) and \( G_{L_2}\) commute. For arbitrary rates \( \kappa_1, \kappa_2\) , their further commutation with \( \kappa_1\, F_{L_1} + \kappa_2\, F_{L_2}\) , as computed in appendix, would generate a sequence of new vector fields in \( \mathfrak{G}_F\) , yielding no efficient model reduction. However, acknowledging the natural setting \( \kappa_1 = \kappa_2 (=1)\) here, while allowing \( \eta_1 \neq \eta_2\) , the commutator with the total deterministic evolution \( \sum_{j=1,2} F_{L_j} + \eta_j D_{L_j}\) yields no other diffusion directions than \( G_{L_1}\) and \( G_{L_2}\) . The 15-dimensional system then remains confined to a 2-dimensional deterministic manifold. This can also be understood by noting that \( F_{L_1} + F_{L_2} = F_{\sigma_{-A}} + F_{\sigma_{-B}}\) . Further variations on the setting are discussed in appendix.
  • One meaningful way to write the actual confining manifold is using the Pauli basis, writing \( \rho_t = \sum_{j,k= I,X,Y,Z} \, r(jk)_t \; \frac\bf{{ \sigma}_{j} \otimes \bf{ \sigma}_k}{4} \; ,\) where \( \sigma_I = \bf{ I}\) the identity, while \( \sigma_X\) , \( \sigma_Y\) , \( \sigma_Z\) are the usual Pauli operators. This is an orthonormal basis for the Frobenius norm, with \( r(jk)_t = \text{Tr}(\rho_t (\bf{ \sigma}_{j} \otimes \bf{ \sigma}_k))\) , in particular \( r(II)_t=1\) for all \( t\) . The dynamics of the 15 other coordinates are obtained by applying the corresponding trace to (15). After defining coordinates \( B_{jk,t} = \frac{r(jk)_t}{r(ZZ)_t-r(IZ)_t-r(ZI)_t}\) , we progressively find \( 13\) linearly independent polynomials, of order \( \leq 3\) in the \( B_{jk,t}\) , which evolve in time independently of the measurement results \( dy_{1,t}\) and \( dy_{2,t}\) , but according to deterministic exponentials in \( t\) .
    The corresponding formulas and proofs are provided in Appendix.

3.3.3 A qudit monitored through \( n\) harmonic oscillators

The first example of Section 3.3.1 can be generalized to the case where the qudit is coupled to \( n>1\) harmonic oscillators, whose fluorescence through \( m\geq 1\) channels is measured. In [66], inspired by [67], the evolution of the system is computed when the harmonic oscillators start in a coherent state and \( m=1\) . It is shown that the harmonic oscillators then remain in a coherent state for all times, with a coherent amplitude that is independent of the measurement outcomes; the stochastic part of the dynamics thus reduces to the \( d^2-1\) variables concerning the qubit, at most. The tools of this note allow us to treat arbitrary initial conditions.

We thus consider the Hilbert space corresponding to \( n\) harmonic oscillators and one qudit. In a rotating frame with respect to the qudit natural Hamiltonian, we consider the following dispersive coupling model:

\[ \begin{eqnarray} d\rho &=&-i\; { \sum_{k=1}^n} \; [ (\Delta_k {\bf a}_k^† {\bf a}_k + u_{t,k} ({\bf a}_k+{\bf a}_k^\dagger) - iv_{t,k} ({\bf a}_k-{\bf a}_k^\dagger) )\,,\; \rho \,] \; dt \end{eqnarray} \]

(16)

\[ \begin{eqnarray} && -i { \sum_{k=1}^n \sum_{j=1}^d}\; \chi_{j,k}\; [|j\rangle\langle j| \otimes {\bf a}_k^† {\bf a}_k\,,\; \rho]\; dt\\ \nonumber && + { \sum_{l=1}^m} \; F_{{\bf b}_l}(\rho)\, dt + \sqrt{\eta_l}\, G_{{\bf b}_l}(\rho)\, dw_{t,l} \; . \\\end{eqnarray} \]

Here \( \bf{ a}_k\) is the annihilation operator of harmonic oscillator \( k=1,2,...,n\) , subsuming tensor product with identity operators; \( \Delta_k, u_k, v_k \in \mathbb{R}\) are detuning and two control signals on oscillator \( k\) ; the qudit has an orthonormal basis \( \{ |j\rangle: j=1,2,...,d \}\) , whose eigenstates are dispersively coupled respectively with strength \( \chi_{j,k} \in \mathbb{R}\) to oscillator \( k\) ; and the whole system decays as it is monitored through the collective modes:

\[ \begin{equation} {\bf b}_{l} = { \sum_{k=1}^n} \; \beta_{l,k} \; {\bf a}_k \; , \end{equation} \]

(17)

with arbitrary coefficients \( \beta_{l,k} \in \mathbb{C}\) for \( l=1,2,...,m\) .

  • Regarding the algebraic criterion of Proposition 1, the \( G_\bf{{ b}_l}\) all commute. As explained in appendix, commutation with the deterministic terms generically yield all vector fields involving the tensor product of some \( |j\rangle\langle j|\) with a complex linear combination of the \( \bf{ a}_k\) ; and, via the drive terms \( u_t, v_t\) , the tensor product of some \( |j\rangle\langle j|\) with \( \mathbf{I}\) or \( i\mathbf{I}\) . The dimension of the manifold, confining the state independently of the measurement results, is thus \( 2 d (n+1)-2\) .

    When \( n\) is small compared to \( d\) , this is less than the \( d^2-1\) variables from [66, 67]; we are thus identifying additional deterministic reduction. When \( n\) is large compared to \( d\) , we have more variables than \( d^2-1\) , thus expressing that general initial conditions yield significantly more complicated dynamics than starting with coherent states. In particular, for a qubit coupled to a single harmonic oscillator as in Section 3.3.1, our general reduced manifold has dimension 6 with controls and dimension 4 for \( u_t=v_t=0\) , compared to dimension \( \leq 3\) for a coherent initial state.

  • Formulas expressing the state \( \rho_t\) at time \( t\) as a function of a reduced number of variables are provided in Appendix. Like for the single resonator, they are based on a Wigner function representation with a Gaussian kernel, whose parameters’ evolution suffices to describe the full state. The stochastic variables essentially concern the Gaussian mean positions and the relative weights of \( \langle j| \rho_t |j\rangle\) , for any qudit level \( j\) . This is consistent with the \( O(nd)\) number of stochastic variables from the algebraic criterion. All the variables governing \( \langle j| \rho_t |j'\rangle\) with \( j'\neq j\) , are deterministically linked to the \( \langle j| \rho_t |j\rangle\) , except for their global phases which (maybe surprisingly) feature some other stochastic degrees of freedom.

    For “sufficiently rich observation” conditions, i.e. ensuring convergence of the Gaussian kernel, the \( n\) -resonator state converges to a product of coherent states \( \prod_{k=1}^n \, |\alpha^{(j,k)}\rangle\) , indexed by and entangled with the qudit levels \( j\) . We then recover the setting of [66, 67]: The coherent state amplitudes \( \alpha^{(j,k)}_t \in \mathbb{C}\) evolve deterministically, i.e. independently of the measurement results. For \( \eta_l \ll 1\) , the total relative weight of levels \( |j\rangle\) , thus \( \text{Tr}(\langle j| \rho_t |j\rangle)\) follow dynamics which coincide with a direct QND measurement of the qudit levels using measurement operators \( L_{l,t} = \sum_{j=1}^d \; \lambda^{(j)}_{l,t} \; |j\rangle\langle j| \, \) , with \( \lambda^{(j)}_{l,t} = {\textstyle \sum_{k=1}^n} \left( \mathfrak{R}(\beta_{l,k})\mathfrak{R}(\alpha^{(j,k)}_t) + \mathfrak{I}(\beta_{l,k})\mathfrak{I}(\alpha^{(j,k)}_t) \right)\; .\)

4 Conclusion

This note provides low-dimensional formulas for the explicit solution of continuously monitored quantum systems, modeled by a nonlinear stochastic differential equation driven by Wiener processes expressing the randomness of measurement results. Covering several typical settings, we show that the state often remains confined to a low-dimensional, deterministically evolving nonlinear manifold, whose equations we compute explicitly. The remaining randomness due to measurement results then only spans a much smaller space, which is often amenable to easier study. This approach can be seen as a generalization of so-called Linear Quantum Systems, where the model can be reduced by sticking to Gaussian states of a set of harmonic oscillators. We here provide low-dimensional expressions for arbitrary states in such systems — admittedly, on the basis of Gaussian kernels, but note that the setting is nonlinear ; and we thus generalize this property to several other, finite-dimensional quantum systems. In other words, whereas in general a single measurement-induced Wiener process can induce diffusion in all dimensions of a quantum system, much like a single control signal can drive a system everywhere in its state space, we here identify many typical systems where this does not happen.

From the viewpoint of representation theory, we are thereby characterizing the minimal memory effect needed, in order to express the results of any future measurements on a quantum system, as a function of all possible values of past measurement signals. Besides its analytical interest, this model reduction can have important practical consequences for efficient parameter estimation, for investigating design options according to measurement statistics [68], and towards writing computationally efficient quantum filters running in real-time for quantum control. Its extension to other quantum filters, including past quantum states, could be envisioned for reducing the complexity of further applications.

The efficiency of our method builds on a simple algebraic criterion, taken from control theory, to check whether low-dimensional confining manifolds exist, and thus whether compact expressions should be available. This criterion allows us to quickly check which variations on a basic setting – like adding a decoherence channel or a Hamiltonian term – retain the property of significant model reduction. It has been key in identifying the parameterizations associated to system (13) for instance, by first indicating the possibility to reduce this particular model, and second telling when we should stop or keep searching for dependencies among the parameters.

Conversely, the results of the algebraic criterion can also be viewed as no-go theorems: it identifies memory effects due to which exact model reduction is sometimes impossible. For instance, in the 3-qubit repetition code with bit-flip channels, an exact reduced filter based on few integrated signals is impossible. Similarly, in the indistinguishable emission case, a condition on the parameters is needed. Finally, in a bipartite system where a single subsystem is monitored, there is no reason to expect confinement to a significantly reduced deterministic manifold in general.

Confining manifolds have been observed in experiments [30, 32], although from a mathematical viewpoint they are not structurally robust. Indeed, even a single generic imperfection Hamiltonian typically generates diffusion in all dimensions under a single stochastic measurement channel. However, the speed of diffusion will be significantly slower in directions corresponding to higher-order commutators of the Hamiltonian with the measurement-induced vector field. This opens several possibilities towards studying approximate confinement, and using it advantageously in approximate (rather than exact) model reduction. In this sense, the treatment of coupled quantum systems or of error correction, or more generally systems featuring significant timescale separations, has only been initiated in this note.

Another point to investigate may be the interaction of measurement backaction with feedback control, i.e. how a particular dependence of control input signals like \( u_t,v_t\) on the output signals \( dy_k\) or on the estimated state, may help reduce the dimension of the confining manifold. Here again, a systematic algebraic criterion should quickly indicate what is feasible or not. Quantum engineering strategies based on the principle of fully countering the stochastic effect with feedback control, have been proposed e.g. in [69].

Finally, while the present note focuses on continuous-time measurements whose backaction is modeled by Wiener processes (typically, field amplitude measurements), a similar study could be imagined for Poisson-type processes ([70, 71], typically photo-detector measurement). While the number of Poisson jumps would lead to a discrete set of options for the measurement-conditioned state, the timing of the jumps could lead to continuous structures in various dimensions.

Acknowledgments

The authors thank Mazyar Mirrahimi, Benjamin Huard, Philippe Campagne-Ibarcq, Vincent Martin, Stefaan De Kesel, Zibo Miao, Paolo Forni, Francesca Chittaro, Philippe Lewalle and Birgitta Whaley for useful discussions. This work was partially supported by the ANR project HAMROQS and by Plan France 2030 through the project ANR-22-PETQ-0006. This work was partially supported by the European Research Council (ERC) under the European Union’s Horizon 2020 research and innovation program (grant agreement No.884762).

6 Appendix

We here give the detailed expressions of the results summarized in the main text, as well as the associated proofs.

Section 6.1 concerns the case of Quantum Non-Demolition Measurement, first general expressions then each of the 3 examples. Section 6.2 contains the cases of harmonic oscillator quadratures measurement, in the same order as in the main text. Section 6.3 concerns bi-partite systems; it gives the full formulas and proofs for the examples of indirect qudit measurement and of indistinguishable emission.

6.1 Appendix 1: Quantum Non-Demolition Measurement

This section contains the details associated to Section 3.1.

6.1.1 General QND expressions

We start with proving the general expressions, first the case of homodyne measurement stated in the main text.

Proof of Proposition 2: We first write the dynamics of each component \( \rho_t(a,b)\) , for instance for the diagonal elements:

\[ \begin{eqnarray} d\rho_t(b,b) & = & \sum_{k=1}^{\bar{k}} \; \sqrt{\eta}_k \left(2 \lambda_k(b) \rho_t(b,b) - ({\textstyle \sum_{a=1}^N \lambda_k(a) \rho_t(a,a)})\, \rho_t(b,b) \right) \, dw_{t,k} \; . \end{eqnarray} \]

(18)

We then look for combinations in which the vector field multiplying each \( dw_k\) cancels. One can quickly check that this is the case for the \( \phi^{(a,b)}\) , \( c^{(a,b)}\) and \( z^{(\alpha)}\) of the statement. Next, the key step towards obtaining the form (5) is to ensure that this set of variables also evolves autonomously: after having established that their dynamics takes the form e.g.

\[ dc^{(a,b)}_t = f(\rho_t) \, dt \; , \]

one must further ensure that \( f(.)\) depends on \( \rho_t\) through only the variables \( \phi^{(a,b)},c^{(a,b)}\) and \( z^{(\alpha)}\) . We have obtained even more, namely independent equations for each variable, e.g.  \( dc^{(a,b)}_t = f\, dt\) with \( f\) depending only on \( c^{(a,b)}_t\) . This is not difficult to check a posteriori. Note that the computation of \( f(\rho_t)\) must use the Itō rule (6). Integration of \( dc^{(a,b)}_t = f(c^{(a,b)}_t) dt\) then yields the result, and similarly for the other variables. \( \square\)

We next generalize to the case of a heterodyne measurement.

Heterodyne QND measurement: For Hermitian \( L_k\) , the output signal \( dy_{t,k}\) associated to \( i L_k\) contains only Wiener noise, independent of the system state. The practical interest of this output channel is thus questionable, but since it is a natural experimental setting for general \( L_k\) , we can quickly treat it for completeness.

Proposition 6

Consider a quantum master SDE (1) on \( \mathcal{H} = \mathbb{C}^N\) , with \( L_k=\sum_{n=1}^N \lambda_k(n) |d_n\rangle\langle d_n|\) in the orthonormal basis \( \{|d_n\rangle\}_{n=1}^N\) and all \( \lambda_k(n)\) real for \( k=1,2,...,\bar{k}/2\) , whereas \( L_{\bar{k}/2+k} = i L_{k}\) . Then the state \( \rho_t\) is restricted to a deterministically evolving manifold of dimension \( \leq \bar{k}\) , characterized by:

\[ \begin{eqnarray*} \phi^{(\beta)}_t & = & \phi^{(\beta)}_0 ~ \text{where } \phi^{(\beta)} = {\textstyle \sum_{a,b=1}^N} \, \beta_{a,b} \, \mathrm{phase}(\rho(a,b)) \\ & & \text{with any } \beta\in\mathbb{R}^{N^2} \text{ solving }\\ & & ~~ \eta_{\bar{k}/2 + k}\textstyle \sum_{a,b=1}^N \beta_{a,b} \, (\lambda_k(a)-\lambda_k(b)) = 0 \;\; \text{for all } k=1,2,...,\bar{k}/2 \; ;\\ c^{(a,b)}_t & = & c^{(a,b)}_0 \, e^{\big( - \overline{(1-\eta)Q_{a,b}^2} \, t \big)} ~ \text{for all } a,b=1,2,...,N \;\;, \\ & & \text{where } \;\;\; c^{(a,b)}_t \; = \; \frac{\vert \rho(a,b) \vert^2}{\rho_t(a,a)\rho_t(b,b)} \\ &&\text{ and } \;\; \overline{(1-\eta)Q_{a,b}^2} = {\textstyle \sum_{k=1}^{\bar{k}}} \; (1-\eta_k) |\lambda_k(a)-\lambda_k(b)|^2 \;\; ; \\ z^{(\alpha)}_t & = & z^{(\alpha)}_0 \, e^{\big( -2 \sigma^2_\alpha \; t \big)} \\ & & \text{where } z^{(\alpha)}_t = \prod_{b=1}^N \, (\rho_t(b,b))^{\alpha_b} \;\; \text{ and } \;\; \sigma^2_\alpha = \sum_{b=1}^N \sum_{k=1}^{\bar k/2} \, \alpha_b \, (\lambda_k(b))^2 \, \eta_k \\ & & \text{with any } \alpha\in\mathbb{R}^N \text{ solving } \textstyle \sum_{b=1}^N \alpha_b = 0 \; ,\\ & & \phantom{ \text{with any } \alpha\in\mathbb{R}^N \text{ solving } } \eta_k \; \textstyle \sum_{b=1}^N \alpha_b \, \lambda_k(b) = 0 \;\; \text{for all } k=1,2,...,\bar{k}/2 \, \; ,\\ & & \phantom{ \text{with any } \alpha\in\mathbb{R}^N \text{ solving } } \text{ and } \sigma^2_\alpha \geq 0 \, . \end{eqnarray*} \]

Proof: The proof is similar to the homodyne case. \( \square\)

The heterodyne setting implies the following modifications with respect to the homodyne case.

  • The set of SDEs governing the diagonal components \( \rho_t(b,b)\) is unaffected by the \( i\, L_k\) , hence the \( z^{(\alpha)}_t\) of Proposition 2 remain valid.
  • The dynamics of \( x^{a,b} := (\rho(a,b)+\rho(b,a))/2\) and \( y^{a,b} := (\rho(a,b)-\rho(b,a))/2i\) are subject to a new noise, associated to a vector field of components \( y^{a,b}_t\) and \( -x^{a,b}_t\) respectively. On one hand, this means that the phases of \( \rho_t(a,b)\) are not preserved anymore but instead follow the random walks:

    \[ d\phi^{(a,b)}_t \; = \; {\textstyle \sum_{k=1}^{\bar{k}/2} }\; (\lambda_k(a)-\lambda_k(b)) \, \sqrt{\eta_k} \, dw_{k+\bar{k}/2\; , \; t} \, . \]

    Those walks are correlated since the system still stays confined in a \( \bar{k}\) -dimensional manifold, and this correlation is expressed by the \( (N^2 - N - \bar{k})/2\) independent variables of type \( \phi^{(\beta)}\) . (Indeed, thanks to \( \rho\) being Hermitian, one checks that the values of \( (\beta_{a,b}+\beta_{b,a})\) , including \( \beta_{a,a}\) for \( a=b\) , have no influence on \( \phi^{(\beta)}\) .)

  • On the other hand, when \( \eta_k<1\) for some \( k>\bar{k}/2\) , the lack of knowledge on phase random walk with respect to someone having access to the full output (\( \eta_k=1\) ), is reflected as a faster decay of off-diagonal elements. More precisely, the deterministic decay still happens on \( c^{(a,b)}\) like in the homodyne case, but with contributions from both parts of the heterodyne channel to the decay rate.

We finally prove the simple explicit expression of the state as a function of measurement results, as stated in Proposition 3.

Proof of Proposition 3: From Itō computations on (18) and recalling the link between \( dw_{k,t}\) and output signal \( dy_{t,k}\) , we obtain the following dynamics for \( r(a,b) := \log(\rho(a,a)/\rho(b,b))\) :

\[ dr_t(a,b) = 2 \sum_{k=1}^{\bar k} \; (\lambda_k(a)-\lambda_k(b)) \sqrt{\eta_k}\, dy_{t,k} - (\lambda_k(a)^2-\lambda_k(b)^2) \eta_k\, dt \; . \]

The right hand side can be trivially integrated, taking its exponential we get:

\[ \left(\frac{\rho(a,a)}{\rho(b,b)}\right)_t = \left(\frac{\rho(a,a)}{\rho(b,b)}\right)_0 \; e^{2 \sum_{k=1}^{\bar k} \; (\lambda_k(a)-\lambda_k(b)) \sqrt{\eta_k}\, y_{t,k} - (\lambda_k(a)^2-\lambda_k(b)^2) \eta_k\, t } \; . \]

This explicit expression is compatible with the stated result. \( \square\)

6.1.2 QND example: Quantum number measurement

Particularizing the above expression to the single measurement channel \( L_1=\sum_{n=0}^{n_{\max}} n \, |n\rangle\langle n|\) , we get the following deterministic variables. For the homodyne case:

  • \( \phi^{(n_1,n_2)}_t =\phi^{(n_1,n_2)}_0\) i.e. the relative phase between coefficients of all photon number states \( |n_1\rangle,|n_2\rangle\) is conserved.
  • \( \dfrac{|\rho_t(n_1,n_2)|^2}{\rho_t(n_1,n_1)\, \rho_t(n_2,n_2)} \, = \, \dfrac{|\rho_0(n_1,n_2)|^2}{\rho_0(n_1,n_1)\, \rho_0(n_2,n_2)}\cdot e^{-(1-\eta)(n_1-n_2)^2\, t}\) , thus the coherence between two different photon numbers decays faster if their numerical difference is larger, which stands in one-to-one correspondence with being more distinguishable in the measurement output.
  • For the diagonal components, we can obtain invariant variables

    \[ \begin{multline*} z^{(\alpha)}_t = z^{(\alpha)}_0 \; \text{ for } \; z^{(\alpha)}=\rho(n_1,n_1)^{\frac{1}{(n_2-n_1)(n_3-n_1)(n_4-n_1)}}\, \rho(n_2,n_2)^{\frac{1}{(n_1-n_2)(n_3-n_2)(n_4-n_2)}} \\ \rho(n_3,n_3)^{\frac{1}{(n_1-n_3)(n_2-n_3)(n_4-n_3)}} \, \rho(n_4,n_4)^{\frac{1}{(n_1-n_4)(n_2-n_4)(n_3-n_4)}}\; . \end{multline*} \]

    This gives the expression reported in the main text when \( (n_2-n_1) = (n_4-n_3)\) .

The characterization through Proposition 3 speaks for itself.

For the heterodyne case, thus \( L_1 = \mathbf{N} \; , \;\; L_2 = i \mathbf{N}\) , the main novelty is that the \( \phi^{(n_1,n_2)}_t\) now undergo correlated random walks. We can write some invariant phase combinations:

\[ \begin{eqnarray*} && \phi^{(\beta)}_t = \phi^{(\beta)}_0 \;\; \text{ for } \\ && ~ \phi^\beta = \text{phase}(\rho(a,b)) - \text{phase}(\rho(a+m,b+m)) \;\; \text{ and for } \\ && ~ \phi^\beta = \tfrac{1}{a+1-b}\, \text{phase}(\rho(a+1,b)) - \tfrac{1}{a-b}\, \text{phase}(\rho(a,b))\; . \end{eqnarray*} \]

In the form (7), we can write the phase evolution with a single stochastic variable \( \gamma_t\) as:

\[ \begin{equation} \text{phase}(\rho_t(a+m,a)) = \text{phase}(\rho_0(a+m,a)) + m\, \gamma_t \;\;\; \text{ for all } a,m\; . \end{equation} \]

(19)

Thus, the further from the diagonal, the more the component is affected by the stochastic phase \( \gamma_t\) .

6.1.3 QND example: continuous-variable measurement

The main text considers a homodyne measurement, we here readily consider the heterodyne case, thus \( L_1 = \mathbf{X}\) and \( L_2 = i \mathbf{X}\) where \( \mathbf{X} = \int_{\mathbb{R}} x\, |x\rangle\langle x| \, dx\) represents for instance the position operator. The expressions are obtained by repeating computations similar to the measurement of \( \mathbf{N}\) and taking the continuous limit.

  • The phases of off-diagonal components feature invariant functions \( \phi^{(\beta)}_t = \phi^{(\beta)}_0\) , including

    \[ \begin{eqnarray*} \phi^{(\beta)} = \tfrac{d}{ds} \mathrm{phase}(\rho(x_1+s,x_2+s)) \;\;& \text{ and } &\;\; \phi^{(\beta)} = \tfrac{d}{dx_1}\left( \frac{1}{x_1-x_2} \mathrm{phase}(\rho(x_1,x_2)) \right) \; . \end{eqnarray*} \]
  • The off-diagonal amplitudes still follow, for all \( x_1,x_2 \in \mathbb{R}\) :

    \[ \begin{eqnarray*} c_t(x_1,x_2) = c_0(x_1,x_2) \, e^{-2(1-\eta)\, (x_1-x_2)^2 \, t} &\;\; \text{ where } \;\; & c(x_1,x_2)\; = \; \frac{\vert \rho(x_1,x_2) \vert ^2}{\rho(x_1,x_1)\rho(x_2,x_2)} \; . \end{eqnarray*} \]

    Thus coherences between positions further apart decay faster. (The factor 2 comes because \( L_1\) and \( L_2\) each contribute.)

  • Regarding the \( z_t^{(\alpha)}\) governing the diagonal components, we obtain the same expressions as in the main text (homodyne case), as \( L_2= i \mathbf{X}\) gives no information on QND level populations.

In the form (7), we can write the phases as:

\[ \begin{equation} \mathrm{phase}(\rho_t(x+s,x)) = \mathrm{phase}(\rho_0(x+s,x)) + s\, \gamma_{t,2} \end{equation} \]

(20)

for all \( x,s \in \mathbb{R}\) , with a single stochastic variable \( \gamma_{t,2}\) independent of \( x,s\) . The distribution \( p(x) = \rho(x,x)\) evolves as for the homodyne case.

6.1.4 QND example: repetition code

The main text mentions that when adding deterministic decoherence channels, associated to spurious bit flips which the code is meant to counter, the confinement to a low-dimensional manifold is lost. To show this, we study the manifold dimension according to Proposition 1. For simplicity of notations, we assume \( \eta_1=\eta_2=\eta_3=\eta\) and \( \gamma_1=\gamma_2=\gamma_3\) .

  • We start with the 3 independent and commuting vector fields \( G_{L_1},G_{L_2},G_{L_3} \in \mathfrak{G}_F\) corresponding to syndrome measurements.
  • The commutator with \( F+\eta D\) yields three new independent vector fields, which we can write using the form (4):

    \[ J_1(\rho) = L_1\, ( \sigma_{2} \rho \sigma_{2} + \sigma_{3} \rho \sigma_{3} + 2 \rho) + ( \sigma_{2} \rho \sigma_{2} + \sigma_{3} \rho \sigma_{x,3} + 2 \rho)\, L_1 \; , \]

    with circular permutation of the indices for \( J_2,J_3\) ; we recall that \( \sigma_k\) denotes a bit-flip (\( \sigma_x\) ) on qubit \( k\) .

  • Since \( \mathfrak{G}_F\) contains the \( J_k\) , it must contain their commutators. This gives 3 new vector fields of the form:

    \[ \begin{eqnarray*} \tilde{J}_{1}(\rho) &=& \sigma_{1} \sigma_{2} \xi \sigma_{1} \sigma_{2} - \sigma_{1} \sigma_{3}\xi \sigma_{1} \sigma_{3} \\ && \text{with } \xi = L_1 \rho + L_2 \rho L_3 + L_3 \rho L_2 + \rho L_1 \; , \end{eqnarray*} \]

    and circular permutation of the indices. The commutators with \( G_{L_k}\) give vector fields:

    \[ \begin{eqnarray*} JG_{1,1}(\rho) &=& (\sigma_{2} \rho \sigma_{2} + \sigma_{3} \rho \sigma_{3}) + L_1\, ( \sigma_{2} \rho \sigma_{2} + \sigma_{3} \rho \sigma_{3}) \, L_1 - 4 \rho \; , \\ JG_{2,3}(\rho) &=& L_1 \xi + L_2 \xi L_3 + L_3 \xi L_2 + \xi L_1 - 4 \text{Trace}(L_1 \rho) \rho \\ && \text{with } \xi = \sigma_{1} \rho \sigma_{1} \; , \end{eqnarray*} \]

    for commutation of \( G_1\) with \( J_1\) and of \( G_3\) with \( J_2\) respectively; to this we add the permutation of the indices.

Checking numerically at various \( \rho\) values, we see that these indeed all provide independent directions, such that the manifold has dimension 15 at least, which is the dimension of two coupled qubits. At this point the model reduction appears quite inefficient at best, so we give up the computation of further commutators.

6.2 Appendix 2: harmonic oscillator quadratures

This section contains the details associated to Section 3.2.

6.2.1 Algebraic criterion and Wigner function

We first investigate the model (10), thus measuring \( L_1=\bf{ a}\) and \( L_2=i \bf{ a}\) , with the algebraic criterion of Proposition 1.

  • We have \( [F_\bf{ a}+\eta_1 D_\bf{ a},\, G_\bf{ a}] = \frac{1}{2} G_\bf{ a}\) , so having only the measurement channels with \( L_1\) and \( L_2\) should yield one- and two-dimensional manifolds, for the homodyne and heterodyne cases respectively.
  • Adding a Hamiltonian in photon number \( \bf{ N} = \bf{ a}^† \bf{ a}\) , its commutation with \( G_\bf{ a}\) yields \( G_{i\bf{ a}}\) , since \( [\bf{ a},\bf{ N}] = \bf{ a}\) . This is understood easily from a physical viewpoint, as a rotation in phase space with Hamiltonian \( \bf{ N}\) transforms \( \bf{ a}\) into \( i\bf{ a}\) . This Hamiltonian has thus no effect on the dimension of \( \mathcal{M}_t\) in the heterodyne case, while in the homodyne case it adds one dimension.
  • When adding dissipation of the form \( F_\bf{{ a}^†}\) , the corresponding commutation with \( G_\bf{ a}\) adds a vector field \( G_\bf{{ a}^†}\) to the algebra \( \mathfrak{G}_F\) , and commutation with \( G_{i \bf{ a}}\) yields the vector field \( G_{i\bf{ a}^†}\) . Those vector fields yield no new terms under further commutation. I.e., when adding deterministic dissipation in \( L_3=\bf{ a}^†\) with \( \eta_3=0\) , the manifold dimension is doubled and no more.
  • Adding a Hamiltonian proportional to \( \bf{ X}\) or \( \bf{ P}\) has no effect on the manifold dimension, in either case. Indeed, e.g. \( [\bf{ a}, 2 \bf{ X}] = [\bf{ a},\bf{ a}^†]=\bf{ I}\) and \( G_{\alpha \bf{ I}}(\rho) = 0\) for all \( \rho\) and all \( \alpha \in \mathbb{C}\) . The same holds when commuting with \( G_{i \bf{ a}}\) , \( G_\bf{{ a}^†}\) , or \( G_{i\bf{ a}^†}\) , if those are present in \( \mathfrak{G}_F\) .

Thus, the measurement outcomes associated to the photon loss channel, in presence of arbitrary drives in \( \bf{ X}\) or \( \bf{ P}\) , can stochastically move the system in 1 dimension (homodyne, no Hamiltonian in \( \bf{ a}^† \bf{ a}\) , zero temperature); in 2 dimensions (homodyne, no Hamiltonian in \( \bf{ a}^† \bf{ a}\) , nonzero temperature; or heterodyne, zero temperature); or in 4 dimensions (heterodyne, nonzero temperature).

We next investigate the algebraic criterion for the model (11), thus measuring \( L_1=\bf{ X}\) and \( L_2 = \bf{ P}\) simultaneously.

  • We have \( [G_\bf{ X},\, G_\bf{ P}] = 0\) because \( G_{[\bf{ X},\,\bf{ P}]} = G_{\alpha \bf{ I}}=0\) for any \( \alpha \in \mathbb{C}\) . From the QND case we already know that \( [F_{L}+\eta D_{L},\, G_{L}]=0\) for both \( L=\bf{ X}\) or \( L=\bf{ P}\) . But we have

    \[ \begin{eqnarray*} [F_{\bf X}+\eta D_{\bf X},\, G_{\bf P}] = G_{i{\bf X}} \;\;&,&\;\; [F_{\bf P}+\eta D_{\bf P},\, G_{\bf X}] = -G_{i{\bf P}} \;\; , \end{eqnarray*} \]

    giving two new vector fields in the Lie algebra. The resulting four vector fields commute and further commutation with \( F_\bf{ X}+\eta D_\bf{ X} + F_\bf{ P}+\eta D_\bf{ P}\) gives no new contributions, so we have found a four-dimensional \( \mathfrak{G}_F\) , accounting for a 4-dimensional manifold.

  • We can add Hamiltonians in \( \bf{ X}\) or \( \bf{ P}\) i.e. typical drives without modifying \( \mathfrak{G}_F\) , like in the above case. We can also add typical imperfection Hamiltonians, proportional to \( \bf{ N}\) or in fact to any linear combination of \( \bf{ X}^2\) and \( \bf{ P}^2\) , since their commutator with \( \mathfrak{G}_F\) gives back vector fields in \( \mathfrak{G}_F\) .
  • When adding photon loss \( L_3\) proportional to \( \bf{ a}\) with \( \eta_3=0\) , the commutation yields a linear combination of \( G_\bf{ X}\) and \( G_\bf{ a}\) , which in turn can be written as a linear combination of \( G_\bf{ X}\) and \( G_{i\bf{ P}}\) . A similar reasoning holds for thermal photons, with \( L_4\) proportional to \( \bf{ a}^†\) with \( \eta_4=0\) .

All these effects can thus be included without pushing the manifold dimension beyond 4.

The main text then focuses on the most general cases (dimension 4 for both examples), expressing the solutions in the form (7). From this, the lower-dimensional manifolds can be obtained as special cases, possibly after a limit computation. (In contrast, when using the form (5), lower-dimensional manifolds require more formulas.)

We choose to describe the state by its Wigner function:

\[ \mathcal{W}^{\{\rho\}}(x,p) = \tfrac{2}{\pi}\,\text{Trace}((-1)^{\bf N}\, {\bf D}_{-(x+ip)}\rho {\bf D}_{x+ip} ) \]

where \( \bf{ D}_\alpha = \exp(\alpha \bf{ a}^† - \alpha^* a)\) is the so-called displacement operator [4], satisfying \( \bf{ D}(\alpha)\, \bf{ a}\, \bf{ D}(\alpha)^\dagger = \bf{ a} - \alpha\) . The Wigner function is a quasi-distribution; it satisfies \( \int\int \mathcal{W}^{\{\rho\}}(x,p) \,dx\,dp= 1\) and, although it is not necessarily positive at each \( (x,p)\) , its marginal \( \; P^{\{\rho\}}(x)= \int \mathcal{W}^{\{\rho\}}(x,p)\,dp \; \) gives the probability distribution associated to \( \rho\) for the operator \( \bf{ X} = \tfrac\bf{{ a}+\bf{ a}^†}{2}\) , and similarly in rotated bases. The SDE on \( \rho\) translates into a stochastic partial differential equation (SPDE) on \( \mathcal{W}^{\{\rho\}}(x,p)\) , with first and second-oder derivatives with respect to \( x\) and \( p\) . Explicitly, to translate a quantum SDE on \( \rho\) to the Wigner function representation, we use the standard properties:

\[ \begin{eqnarray*} \mathcal{W}^{\{{\bf a}^† \rho\}} = \left( (x-ip) - \tfrac{1}{4}(\tfrac{\partial}{\partial x}-i\tfrac{\partial}{\partial p})\right) \mathcal{W}^{\{\rho\}} &,&\;\; \mathcal{W}^{\{{\bf a} \rho\}} = \left( (x+ip) + \tfrac{1}{4}(\tfrac{\partial}{\partial x}+i\tfrac{\partial}{\partial p})\right) \mathcal{W}^{\{\rho\}}\; ,\\ \mathcal{W}^{\{\rho {\bf a}\}} = \left( (x+ip) - \tfrac{1}{4}(\tfrac{\partial}{\partial x}+i\tfrac{\partial}{\partial p})\right) \mathcal{W}^{\{\rho\}} &,& \;\; \mathcal{W}^{\{\rho {\bf a}^†\}} = \left( (x-ip) + \tfrac{1}{4}(\tfrac{\partial}{\partial x}-i\tfrac{\partial}{\partial p})\right) \mathcal{W}^{\{\rho\}}\; . \end{eqnarray*} \]

For \( \eta=0\) , the SPDE becomes a linear deterministic PDE that can be solved with a Gaussian, time-varying Green function which is separable in the \( x\) and \( p\) variables. Under measurements, the same representation stays rather efficient, although the Gaussian kernel undergoes a somewhat more complicated evolution.

6.2.2 Full expressions for measurement of \( \bf{ a}\) and \( i \bf{ a}\)

We now characterize the deterministic manifold corresponding to the model (10). We first re-state Proposition 4 with all details.

Proposition 7

The quantum SDE (10), taking \( \Delta=0\) without loss of generality, admits the following explicit solution:

\[ \mathcal{W}^{ \{\rho\} }_t(x,p) = \int \int \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\, K_{x,t}(x,x_0)\, K_{p,t}(p,p_0) \, dx_0\, dp_0\; \nu_t \]

where \( \nu_t\) is a normalization constant and

\[ \begin{eqnarray*} K_{x,t}(x,x_0) &=& \exp\left( \frac{-(x-x_0 a_t - \xi_t)^2}{s_t} + (d_t\, x_0^2+\theta_{t}x_0) \right)\;\; , \\ K_{p,t}(p,p_0) &=& \exp\left( \frac{-(p-p_0 a_t - \pi_t)^2}{s_t} + (d_t\, p_0^2+\phi_{t}p_0) \right)\;\;. \end{eqnarray*} \]

These functions involve the deterministic time-dependent variables:

\[ \begin{eqnarray*} a_t &=& \frac{2 \kappa e^{-\kappa t}}{(\kappa+1-\eta) + (\kappa-1+\eta)e^{-2\kappa t}} \\ s_t &=& \frac{-(1-\eta)}{2\eta} + \frac{\kappa}{2\eta} \frac{1-\frac{\kappa-1+\eta}{\kappa+1-\eta} e^{-2\kappa t}}{1+\frac{\kappa-1+\eta}{\kappa+1-\eta} e^{-2\kappa t}}\\ d_{t} &=& \frac{2\eta(e^{-2\kappa t}-1)}{(\kappa+1-\eta) + (\kappa-1+\eta)e^{-2\kappa t}} \end{eqnarray*} \]

where \( \kappa = \sqrt{1 + 4 \eta\, n_{th}}\) . Thus \( \mathcal{W}^{\{\rho\}}_t(x,p)\) depends on the measurement results only through the four parameters:

\[ \begin{eqnarray} d\xi_t &=& \sqrt{\eta}(s_t-\frac{1}{2})\, dy_{t,1} + \left(v_t - \xi_t - 2 \eta(s_t-\tfrac{1}{2})\, \xi_t \right) \, dt \end{eqnarray} \]

(21)

\[ \begin{eqnarray} d\theta_t &=& 2\sqrt{\eta} a_t\, dy_{t,1} - 4 \eta\, a_t \xi_t \, dt\\ \nonumber d\pi_t &=& \sqrt{\eta}(s_t-\frac{1}{2})\, dy_{t,2} + \left(-u_t - \pi_t - 2 \eta(s_t-\tfrac{1}{2})\, \pi_t \right) \, dt \\ \nonumber d\phi_t &=& 2\sqrt{\eta} a_t\, dy_{t,2} - 4 \eta\, a_t \pi_t \, dt \, , \\\end{eqnarray} \]

initialized with \( \xi_0=\theta_0=\pi_0=\phi_0 = 0\) .

Moreover, for \( n_{th}=0\) , the model can be further reduced, keeping only two stochastic variables, as the set of equations (21) becomes equivalent to:

\[ \begin{eqnarray*} d\xi_t &=& \sqrt{\eta}(s_t-\frac{1}{2})\, dy_{t,1} + \left(v_t - \xi_t - 2 \eta(s_t-\tfrac{1}{2})\, \xi_t \right) \, dt \\ d\pi_t &=& \sqrt{\eta}(s_t-\frac{1}{2})\, dy_{t,2} + \left(-u_t - \pi_t - 2 \eta(s_t-\tfrac{1}{2})\, \pi_t \right) \, dt \\ \frac{dz_t}{dt}&=& v_t - z_t ~ \text{ for } z_t= \xi_t + \tfrac{e^{-t}}{4}\, \theta_t \\ \frac{dh_t}{dt}&=& - u_t - h_t ~ \text{ for } h_t= \pi_t + \tfrac{e^{-t}}{4}\, \phi_t \, .\\ \end{eqnarray*} \]

Proof: To prove Proposition 7, we start by converting (10) with \( \Delta=0\) to an SPDE on the Wigner representation:

\[ \begin{eqnarray} d\mathcal{W} &=& 2 \sqrt{\eta} \left( x + \tfrac{1}{4} \frac{\partial}{\partial x} - \bar{x}_{\mathcal{W}} \right)\, \mathcal{W}\, dw^1_t \end{eqnarray} \]

(22)

\[ \begin{eqnarray} & & - 2 \sqrt{\eta} \left(p + \tfrac{1}{4} \frac{\partial}{\partial p} - \bar{p}_{\mathcal{W}} \right)\, \mathcal{W}\, dw^2_t \\ & & + \left( 1 + (x-v_t)\frac{\partial}{\partial x} + \frac{1+2 n_{th}}{4}\frac{\partial^2}{\partial x^2} \right) \, \mathcal{W}\, dt \\ \nonumber & & + \left(1 + (p + u_t)\frac{\partial}{\partial p} + \frac{1+2 n_{th}}{4}\frac{\partial^2}{\partial p^2}\right) \, \mathcal{W}\, dt \; ,\\ \\\end{eqnarray} \]

where \( \bar{x}_{\mathcal{W}} = \int\int x \mathcal{W}(x,p) \, dx\, dp\) and \( \bar{p}_{\mathcal{W}} = \int\int p \mathcal{W}(x,p) \, dx\, dp\) .

We observe that this equation splits into one part in \( x\) and one part in \( p\) ; since those two parts are subject to independent noises, there is no cross-term in the Itō correction. We will thus try to express the solution with a factorized Green function \( K_{x,t} \; K_{p,t}\) as in the statement, and search for an expression of \( K_{x,t}\) that satisfies the \( x\) -part of the equation, for any \( p\) and any \( V_p(x,x_0) = \int \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\, K_{p,t}(p,p_0)\, dp_0\) ; the expression of \( K_{p,t}\) is then deduced by symmetry.

Using the Gaussian parameterization of \( K_{x,t} \sqrt{\nu_t}\) as stated the Proposition, we get an expression for the \( x\) -part on the right-hand side of (22) as a function of the parameters \( a_t,s_t,d_t,\xi_t,\theta_t\) and \( \sqrt{\nu_t}\) ; note that \( \bar{x}(\mathcal{W})\) here becomes just a particular function of the parameters and of \( \mathcal{W}^{\{\rho\}}_0\) . The left-hand side is expressed with the time variations \( da_t,...,\, d\theta_t,\, d\nu_t\) , including their squares as required by Itō calculus. Equating the same powers of \( x\) and \( x_0\) inside the integrals on the left- and right-hand side, and the terms in \( dt\) or \( dw^1_t\) respectively, yields a set of equations which turn out to have a solution.

One first checks, equating the terms proportional to \( dw^1_t\) and to various powers of \( x,x_0\) , that \( da_t,\, ds_t,\, dd_t\) should involve no noise term, while \( d\xi_t\) , \( d\phi_t\) and \( d\nu_t\) include a noise term. Next, from the \( x^2\, dt\) term, we get a nonlinear ODE for \( s_t\) :

\[ \frac{ds_t}{dt} + 2 \eta (s_t-\tfrac{1}{2})^2 = -2 s_t + (1+2 n_{th})\, . \]

This is in Ricatti form and can be integrated with standard methods, e.g. relating \( s_t\) to \( \frac{\dot{u}_t}{u_t}\) where \( u_t\) is a mathematical auxiliary signal. After thus solving this equation for \( s_t\) , we get similar first-order ODEs for \( a_t\) (containing \( s_t\) ) and for \( d_t\) (containing \( a_t\) ) respectively from the term in \( x x_0\) and from the term in \( x_0^2\) . Expressing the ODE for \( a_t\) with the Ricatti auxiliary signal \( u_t\) from the \( s_t\) equation yields a quick solution, while the \( d_t\) equation admits explicit integration. Finally, the terms in \( x\) and \( x_0\) yield the SDEs for \( \xi_t\) and \( \theta_t\) given in the Proposition statement. We do not need to compute the SDE for \( \nu_t\) since we know beforehand that, as a normalization constant, it will have an expression as a function of the other parameters and of \( \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\) . It was important however to include it in the equations in order to compute the Itō correction correctly. The requirement \( \mathcal{W}^{\{\rho\}}_0(x,p) = \int \int \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\, K_{x,0}(x,x_0)\, K_{p,0}(p,p_0) \, dx_0\, dp_0\; \nu_0\) allows to fix the initial values of all the parameters’ differential equations.

Concerning \( K_{p,t}(p,p_0)\) , since the equations for the deterministic variables are exactly the same, we can use the same parameters \( a_t,s_t,d_t\) ; the stochastic variables of course must be taken different, since they will evolve according to different Wiener processes. \( \square\)

Special case \( n_{th}=0\) :

According to the algebraic criterion, in this case the number of stochastic variables is supposed to decrease. This can be confirmed on our Wigner representation, by checking the algebraic criterion now for the classical SDE governing the evolution of the 3-dimensional system \( \xi_t,\theta_t\) and \( t\) . The variable \( t\) must be explicitly included since the expressions are all explicitly time-dependent through \( a_t,s_t,d_t\) . The Stratonovich form is identical to the Itō form, because the Wiener vector field only depends on \( t\) , which itself has no stochastic evolution (\( dt = 1 \cdot dt + 0 \cdot dw^1_t\) ). Then the commutator of the deterministic vector field with the Wiener vector field, turns out indeed to be proportional to the Wiener vector field itself (no new direction), if and only if \( n_{th}=0\) . In other words, the variables \( \xi_t,\theta_t\) remain confined to a one-dimensional manifold. For \( n_{th}>0\) a new component appears in the commutator, confirming that in this case the pair of variables \( (\xi_t,\theta_t)\) driven by a single Wiener process \( dw^1_t\) , can diffuse to span the entire plane at any given time \( t\) , and can thus not be further reduced.

We can parameterize the time-dependent curve to which \( \xi_t,\theta_t\) are confined for \( n_{th}=0\) , by saying that a combination \( z_t(\xi_t,\theta_t,t)\) of the variables (not reduced to \( z_t=t\) ) must evolve deterministically. Canceling the contribution of \( dw^1_t\) in \( dz\) leads to the constraint \( \tfrac{\partial z_t}{\partial \xi} = 4 e^t\, \tfrac{\partial z_t}{\partial \theta}\) . This suggests the solution \( z_t = 4 \xi_t + e^{-t} \theta_t\) . We further check that the evolution of such \( z_t\) is deterministic, i.e. the right-hand side of

\[ \tfrac{d}{dt}z_t(\xi_t,\theta_t,t) = 4 e^t\, \tfrac{\partial z_t}{\partial \theta}\, (v_t - \xi_t) + \tfrac{\partial z_t}{\partial t}\; , \]

depends only on \( z_t\) and on \( t\) . (Of course this solution is far from unique as any function of \( z_t\) and \( t\) would also be a solution.) \( \square\)

6.2.3 Full expressions for measurement of \( \bf{ X}\) and \( \bf{ P}\)

We now characterize the deterministic manifold corresponding to the model (11). We first re-state Proposition 5 with all details.

Proposition 8

The quantum SDE (11) admits the following explicit solution:

\[ \mathcal{W}^{\{\rho\}}_t(x,p) = \int \int \mathcal{W}^{\{\rho\}}_0(x_0,p_0)\, K_{t}(x,x_0,p,p_0)\, dx_0\, dp_0\; \nu_t \]

where \( \nu_t\) is a normalization constant and

\[ \begin{eqnarray*} K_{t}(x,x_0,p,p_0) &=& \exp\big[ -(q-A_t x_0 - R_t p_0 - \Theta_t)^T (S_t)^{-1} (q-A_t x_0 - R_t p_0 - \Theta_t)\\ && ~ ~~ + (q_0)^T Z_t q_0 + (\Lambda_t)^T (\, A_t \;,\; R_t \,)\, q_0 \big]\; , \\ \end{eqnarray*} \]

with column vectors \( q = (x \,; \; p) \in \mathbb{R}^2\) and \( q_0 = (x_0 \,; \; p_0) \in \mathbb{R}^2\) . The \( 2 \times 2\) matrices \( S_t\) and \( Z_t\) are symmetric and evolve deterministically as:

\[ \begin{eqnarray*} \tfrac{d}{dt}S_t &=& -\Gamma_\ell\, S_t + \tfrac{(1+2n_{th}) \Gamma_\ell}{2} I - 2 S_t \, M_t \, S_t + \tfrac{1}{2}N_t \\ \tfrac{d}{dt}Z_t &=& - 2 \, \left(\begin{array}{c} (A_t)^T \\ (R_t)^T \end{array} \right) \, M_t \, \left(\begin{array}{cc} A_t \, ,& R_t \end{array} \right) \\ && \text{with }\;\; M_t = \left(\begin{array}{cc} \eta_x \Gamma_x \cos^2(\Delta t) + \eta_p \Gamma_p \sin^2(\Delta t) & (\eta_x \Gamma_x - \eta_p \Gamma_p) \sin\cos(\Delta t) \\ (\eta_x \Gamma_x - \eta_p \Gamma_p) \sin\cos(\Delta t) & \eta_p \Gamma_p \cos^2(\Delta t) + \eta_x \Gamma_x \sin^2(\Delta t) \end{array}\right) \\ && \text{and } \;\;\;\; N_t = \left(\begin{array}{cc} \Gamma_p \cos^2(\Delta t) + \Gamma_x \sin^2(\Delta t) & (\Gamma_p - \Gamma_x) \sin\cos(\Delta t) \\ (\Gamma_p - \Gamma_x) \sin\cos(\Delta t) & \Gamma_x \cos^2(\Delta t) + \Gamma_p \sin^2(\Delta t) \end{array}\right) \; , \end{eqnarray*} \]

starting from initial conditions \( S_0 = Z_0 = 0\) . The column vectors \( A_t,\; R_t \in \mathbb{R}^2\) follow the independent linear ODEs:

\[ \begin{eqnarray*} \tfrac{d}{dt} A_t & = & \tfrac{-\Gamma_l}{2} A_t - 2 S_t \, M_t \, A_t \\ \tfrac{d}{dt} R_t & = & \tfrac{-\Gamma_l}{2} R_t - 2 S_t \, M_t \, R_t \; , \end{eqnarray*} \]

starting from initial conditions \( A_0 = (\, 1 \;,\; 0 \,)^T\) and \( R_0 = ( \, 0 \;,\; 1 \, )^T\) . Thus \( \mathcal{W}^{ \{ \rho\} }_t(x,p)\) depends on the measurement results only through 2 column vectors in \( \mathbb{R}^2\) which follow the linear, block-triangular set of SDEs:

\[ \begin{eqnarray*} d\Theta_t &=& \left( \tfrac{-\Gamma_\ell}{2} \Theta_t + \left(\begin{array}{c} v_t \\ -u_t \end{array} \right) - 2 S_t\, M_t \, \Theta_t \right) \, dt \\ && + S_t \, \left(\begin{array}{c} \sqrt{\eta_x \Gamma_x} \cos(\Delta t)\, dy_{t,1} - \sqrt{\eta_p \Gamma_p} \sin(\Delta t)\, dy_{t,2} \\ \sqrt{\eta_x \Gamma_x} \sin(\Delta t)\, dy_{t,1} + \sqrt{\eta_p \Gamma_p} \cos(\Delta t)\, dy_{t,2} \end{array} \right) \\ d\Lambda_t &=& \left( \tfrac{\Gamma_\ell}{2} \Lambda_t + 2 M_t \, S_t \Lambda_t - 4 M_t\, \Theta_t \right) \, dt \\ && + 2\, \left(\begin{array}{c} \sqrt{\eta_x \Gamma_x} \cos(\Delta t)\, dy_{t,1} - \sqrt{\eta_p \Gamma_p} \sin(\Delta t)\, dy_{t,2} \\ \sqrt{\eta_x \Gamma_x} \sin(\Delta t)\, dy_{t,1} + \sqrt{\eta_p \Gamma_p} \cos(\Delta t)\, dy_{t,2} \end{array} \right) \; , \end{eqnarray*} \]

starting from initial conditions \( \Theta_t = \Lambda_t = 0\) . These SDEs on \( \mathbb{R}^4\) , driven by 2 noise processes, lead in general to diffusion in all 4 dimensions at any given time \( t>0\) .

Proof: The dynamics (11) translates to the Wigner function as follows:

\[ \begin{eqnarray} d\mathcal{W} &=& 2 \sqrt{\eta_x\Gamma_x} \left( 2(x - \bar{x}(\mathcal{W}))\cos(\Delta t) + 2(p - \bar{p}(\mathcal{W}))\sin(\Delta t) \right) \mathcal{W}\, dw^1_t \end{eqnarray} \]

(23)

\[ \begin{eqnarray} && + \sqrt{\eta_p\Gamma_p} \left( 2(p - \bar{p}(\mathcal{W}))\cos(\Delta t) - 2(x - \bar{x}(\mathcal{W}))\sin(\Delta t) \right) \mathcal{W}\, dw^2_t\\ \nonumber && + \frac{\Gamma_\ell}{2} \left(2 + x \tfrac{\partial}{\partial x} + p\tfrac{\partial}{\partial p} + \tfrac{1 + 2 n_{th}}{4} (\tfrac{\partial^2}{\partial x^2} + \tfrac{\partial^2}{\partial p^2}) \right) \, \mathcal{W} \, dt \\ \nonumber && + \left( -v_t\, \tfrac{\partial}{\partial x} + u_t\, \tfrac{\partial}{\partial p} \right) \, \mathcal{W} \, dt \\ \nonumber && + (\tfrac{\Gamma_x \cos^2(\Delta t)}{8} + \tfrac{\Gamma_p \sin^2(\Delta t)}{8}) \tfrac{\partial^2}{\partial p^2} \mathcal{W} \, dt + (\tfrac{\Gamma_x \sin^2(\Delta t)}{8} + \tfrac{\Gamma_p \cos^2(\Delta t)}{8}) \tfrac{\partial^2}{\partial x^2} \mathcal{W} \, dt \\ \nonumber && + \tfrac{\Gamma_p-\Gamma_x}{4} \sin\cos(\Delta t) \tfrac{\partial^2}{\partial x \, \partial p} \mathcal{W} \, dt \; , \\\end{eqnarray} \]

where again \( \bar{x}(\mathcal{W}) = \int\int x \mathcal{W}(x,p) \, dx\, dp\;\) and \( \; \bar{p}(\mathcal{W}) = \int\int p \mathcal{W}(x,p) \, dx\, dp\) .

This SPDE contains a coupling between \( x\) and \( p\) variables through a term proportional to \( \tfrac{\partial^2}{\partial x \partial p}\) , expressing that there is a rotation at rate \( \Delta\) between the diffusion principal axes and our coordinate frame. As a consequence, the equation now does not separate in \( x\) and \( p\) , so we introduce the joint Green function \( K_t(x,x_0,p,p_0)\) . (This coupling has also prevented us from readily integrating the deterministic equations, we come back to special cases below.) Similarly to Proposition 7, we then express \( d\mathcal{W}\) , on one hand from the right-hand side of (23), and on the other hand from infinitesimal variations in the parameters of \( K_t(x,x_0,p,p_0)\) with the form postulated in Proposition 8 as an Ansatz; for the latter we must go up to second order (Itō correction) for the parameters whose evolution involves a noise term. Equating the same powers of \( x,\,p,\,p_0\) and \( x_0\) inside the integrals on the left and right side, and the terms in \( dw^1_t,\, dw^2_t\) or \( dt\) respectively, yields the set of equations which we set out to solve.

We first check the matching of terms in \( dw^1_t,\, dw^2_t\) . Starting with the \( x^2\) , \( p^2\) and \( xp\) terms we see that \( dS_t\) must be proportional to \( dt\) , with no component proportional to \( dw^1_t,\, dw^2_t\) . This also simplifies the other equations, as there is no second-order Itō term from \( dS_t\) . Then considering terms in \( xx_0\) , \( xp_0\) , \( px_0\) and \( pp_0\) yields the same conclusion for \( A_t, R_t\) . After this, the terms in \( x_0^2\) , \( p_0^2\) and \( x_0 p_0\) give the same conclusion for \( Z_t\) . Next, the terms proportional to \( dy_{1,t}\) and \( dy_{2,t}\) in the equations for \( \Theta_t\) are obtained from the terms in \( x,\,p\) . From there the contributions to \( \Lambda_t\) are obtained with the terms in \( x_0,\,p_0\) . Finally, the term proportional to \( 1\) yields the contribution to the normalizing constant \( \nu_t\) , which must just be taken into account for the Itō correction.

After this, we consider the terms proportional to \( dt\) , to obtain the deterministic contributions to the equations. Only few parameters contribute to the second-order Itō correction. We consider the coefficients in the same order as for the noise investigation, starting with \( x^2\) and so on. It helps to use \( Q_t = (S_t)^{-1}\) as an intermediate variable. One can check, using the algebraic criterion on the vector fields for the system \( \Theta_t,\Lambda_t\) , that in general it indeed yields diffusion in all 4 dimensions and thus cannot be reduced further. \( \square\)

We can explicitly write down the result for some special cases where the equations simplify.

For \( \Gamma_x = \Gamma_p\) and \( \eta_x = \eta_p\) , the model is invariant under a rotation; in other words, in this situation it is equivalent to assume \( \Delta=0\) . In both these cases, the \( x\) and \( p\) variables can be separated and we get the following simpler expressions, although the manifold remains of dimension 4.

Corollary 1

For \( \Delta=0\) or for \( (\Gamma_x\, ,\, \eta_x) = (\Gamma_p\, ,\, \eta_p)\) , the solution of Proposition 8 allows the following integration of the deterministic parameters:

  • \( S_t=\text{diag}(\,s_{1,t}\; , \; s_{2,t}\,)\) and \( Z_t=\text{diag}(\,z_{1,t}\; , \; z_{2,t}\,)\) are diagonal. Defining
    \( \kappa_1 = \sqrt{\tfrac{\Gamma_\ell^2}{4}+\tfrac{\Gamma_\ell(1+2n_{th}+\Gamma_p)}{2}}\) and \( \kappa_2 = \sqrt{\tfrac{\Gamma_\ell^2}{4}+\tfrac{\Gamma_\ell(1+2n_{th}+\Gamma_x)}{2}}\) , we have

    \[ \begin{eqnarray*} s_{1,t} &=& \tfrac{\Gamma_\ell(1+2n_{th}+\Gamma_p)}{4 \eta_x \Gamma_x}\; \frac{e^{\kappa_1 t} - e^{-\kappa_1 t}}{(\kappa_1+\Gamma_\ell/2) e^{\kappa_1 t} + (\kappa_1-\Gamma_\ell/2) e^{-\kappa_1 t}}\\ s_{2,t} &=& \tfrac{\Gamma_\ell(1+2n_{th}+\Gamma_x)}{4 \eta_p \Gamma_p}\; \frac{e^{\kappa_2 t} - e^{-\kappa_2 t}}{(\kappa_2+\Gamma_\ell/2) e^{\kappa_2 t} + (\kappa_2-\Gamma_\ell/2) e^{-\kappa_2 t}} \;\; , \\ z_{1,t} &=& \frac{2 \eta_x \Gamma_x (e^{-2 \kappa_1 t}-1)}{(\kappa_1+\Gamma_\ell/2) + (\kappa_1-\Gamma_\ell/2) e^{-2\kappa_1 t}} \\ z_{2,t} &=& \frac{2 \eta_p \Gamma_p (e^{-2 \kappa_2 t}-1)}{(\kappa_2+\Gamma_\ell/2) + (\kappa_2-\Gamma_\ell/2) e^{-2\kappa_2 t}} \; . \end{eqnarray*} \]
  • The vectors \( A_t\) and \( R_t\) \( \in \mathbb{R}^2\) feature \( a_{2,t} = r_{1,t} = 0\) , while

    \[ \begin{eqnarray*} a_{1,t} &=& \frac{2 \kappa_1\, e^{-\kappa_1 t}}{(\kappa_1+\Gamma_\ell/2) + (\kappa_1-\Gamma_\ell/2) e^{-2\kappa_1 t}}\\ r_{2,t} &=& \frac{2 \kappa_2\, e^{-\kappa_2 t}}{(\kappa_2+\Gamma_\ell/2) + (\kappa_2-\Gamma_\ell/2) e^{-2\kappa_2 t}} \, . \end{eqnarray*} \]
  • The stochastic variables decouple into two independent sets of equations for \( (\theta_{1,t}\;,\;\lambda_{1,t})\) and for \( (\theta_{2,t}\;,\;\lambda_{2,t})\) respectively.

Proof: The term in \( \tfrac{\partial^2}{\partial x \partial p}\) vanishes in the SPDE of the Wigner function, thus in fact the \( x\) and \( p\) variables can effectively be separated, like in Proposition 7. In the expressoins of Proposition 8, this translates into decoupled equations. We first note that the matrices \( M_t\) and \( N_t\) become diagonal. From this and the initial condition \( S_0=0\) , we have that \( S_t\) is diagonal. For \( \eta_x \Gamma_x\, \eta_p \Gamma_p \neq 0\) , the equations for the diagonal elements of \( S_t\) take a Ricatti form which can be integrated. As a consequence, the elements of \( A_t\) and \( R_t\) follow 4 independent equations. From the initial conditions, the matrix \( (A_t \; ; \; R_t)\) is diagonal and the components can be integrated once knowing \( S_t\) . Then a similar procedure allows to integrate \( Z_t\) , leading to the result. \( \square\)

Finally, we can link back to Section 3.1. Setting \( \Gamma_p=0\) in Proposition 8, we obtain the result for QND measurement of \( \bf{ X}\) , but now in presence of detuning and thermal environment. When the latter take the most general values, the algebraic criterion still predicts an SDE on 4 scalars, thus diffusion on a 4-dimensional manifold under this single measurement channel. As announced in the main text, the manifold dimension reduces e.g. for the particular case \( \Delta=0\) with \( \Gamma_p = 0\) , and we obtain the following particular formulas.

Corollary 2

For \( \eta_p \Gamma_p = 0\) and \( \Delta=0\) , the dependence of the solution of Proposition 8 on the measurement signal reduces to a 2-dimensional SDE, whereas we get the following particular deterministic parameter evolutions:

\[ \begin{eqnarray*} s_{2,t} &=& \tfrac{\Gamma_x + \Gamma_\ell(1+2n_{th})}{2 \Gamma_\ell}\,(1 - e^{-\Gamma_\ell t}) \\ r_{2,t} &=& e^{-\Gamma_\ell t/2} \; , ~~ z_{2,t} \;=\; 0 \\ \theta_{2,t} &=& \int_0^t -u_s\, e^{-(t-s)\Gamma_\ell/2} \, ds \; , ~ \lambda_{2,t} = 0 \; . \end{eqnarray*} \]

The other parameters are obtained by plugging \( \eta_p \Gamma_p = 0\) into Corollary 1 or Proposition 8.

Proof: The proof is similar to the previous cases. Compared to Corollary 1, the equation for \( s_{1,t}\) does not take a Ricatti form anymore but it becomes affine. This yields the different form for the explicit solution. \( \square\)

6.3 Appendix 3: bipartite quantum systems

This section contains the details associated to Section 3.3.

6.3.1 Indirect qudit measurement

We start by detailing the investigation with the algebraic criterion, before giving the full expression of the associated manifold. The results are given for a non-degenerate coupling operator \( Q_A = \sum_{s=1}^d \, \lambda_s \, |s\rangle\langle s|\) ; generalizing to a degenerate one involves no particular complications.

Proposition 9

The system (13) features deterministic manifolds \( \mathcal{M}_t\) of dimension \( 4 d - 2\) , characterized by the Abelian algebra:

\[ \mathfrak{G}_F = \text{span}\{G_{|s\rangle\langle s| \otimes \delta {\bf b}} : s=1,2,...,d;\; \delta =1,i \} \cup \{ G_{|s\rangle\langle s| \otimes \delta {\bf I}} : s=1,2,...,d-1;\; \delta =1,i \} \; . \]

In absence of drives, thus for \( u_t=v_t=0\) , the manifold further reduces to dimension 2d, characterized by the Abelian algebra:

\[ \mathfrak{G}_F = \text{span}\{G_{|s\rangle\langle s| \otimes \delta {\bf b}} : s=1,2,...,d;\; \delta =1,i \} \; . \]

Proof: Note that we check commutation with each of the deterministic vector fields independently, as they involve a priori independent scales and should thus allow to span their respective directions independently.

  • - The operators acting on B alone give an algebra \( \mathfrak{G}_B = \text{span}\{\, G_\bf{ b}\,,\; G_{i\bf{ b}} \, \} \; .\)
  • -

    The commutation with \( G_{-i\,Q_A \otimes (\bf{ b}^† \bf{ b})}\) yields two new vector fields

    \[ G_{Q_A \otimes {\bf b}} \;\;\; \text{ and } \;\;\; G_{iQ_A \otimes {\bf b}} \; . \]

    Those commute with the elements of \( \mathfrak{G}_B\) , we just have to check further commutation with the terms of the deterministic vector field. Commutation with \( F_\bf{ b} = F_{i\bf{ b}}\) yields no new term. Commutation with the drives yields

    \[ G_{Q_A \otimes {\bf I}} \;\;\; \text{ and } \;\;\; G_{iQ_A \otimes {\bf I}} \; . \]
  • -

    From here we can proceed by induction. Assume that we have the Abelian algebra of vector fields:

    \[ \mathfrak{G}_{\bar{s}} := \text{span}\{ G_{Q_A^{s-1} \otimes {\bf b}} \; ,\; G_{i Q_A^{s-1} \otimes {\bf b}} \; ,\; G_{Q_A^{s-1} \otimes {\bf I}} \; ,\; G_{i Q_A^{s-1} \otimes {\bf I}} \;\; : \;\; s=1,2,...,\bar{s} \} \; . \]

    Then one commutation with the vector fields associated to the drive Hamiltonian, the coupling Hamiltonian and \( F_\bf{ b} + \eta D_\bf{ b}\) yields the Abelian algebra \( \; \mathfrak{G}_{\overline{s+1}} \; \) . Similarly, in absence of drives, consider the Abelian algebra of vector fields:

    \[ \tilde{\mathfrak{G}}_{\bar{s}} := \text{span}\{ G_{Q_A^{s-1} \otimes {\bf b}} \; ,\; G_{i Q_A^{s-1} \otimes {\bf b}} \;\; : \;\; s=1,2,...,\bar{s} \} \; . \]

    Then one commutation with the vector field associated to the coupling Hamiltonian and \( F_\bf{ b} + \eta D_\bf{ b}\) yields the Abelian algebra \( \; \tilde{\mathfrak{G}}_{\overline{s+1}} \; \) .

    The iteration stops once \( \mathfrak{G}_{\overline{s+1}} = \mathfrak{G}_{\bar{s}} \; \) , which for a \( d\) -dimensional (non-degenerate) Hermitian matrix \( Q_A\) holds once \( \bar{s} \geq d\) .

From here the result follows by equivalence of \( \text{span}\{ G_{Q_A^s \otimes \bf{ Q}} : s=1,2,...,d \}\) and \( \text{span}\{ G_{|s\rangle\langle s| \otimes \bf{ Q}} : s=1,2,...,d \}\) for any operator \( \bf{ Q}\) . For \( \bf{ Q} = \alpha \bf{ I}\) a complex multiple of identity, since \( G_{\alpha I \otimes \bf{ I}} = 0\) , we further have \( \text{span}\{ G_{|s\rangle\langle s| \otimes \alpha\bf{ I}} : s=1,2,...,d \} = \text{span}\{ G_{|s\rangle\langle s| \otimes \alpha \bf{ I}} : s=1,2,...,d-1 \}\) . \( \square\)

Although the control signals are deterministic, they can a priori take any forms, and therefore the following result will further motivate the Ansatz for writing the actual manifold equations.

Proposition 10

The set of states reachable by system (13), under all measurement realizations and all control signals \( u_t,v_t\) , is confined to a time-dependent manifold \( \tilde{\mathcal{M}}_t\) of dimension \( 3 d^2 +2d - 1\) , characterized by the algebra:

\[ \begin{eqnarray} \mathfrak{G}_F &=& \text{span}\{G_{|s\rangle\langle s| \otimes {\bf I}} : s=1,2,...,d-1 \} \end{eqnarray} \]

(24)

\[ \begin{eqnarray} && \cup \{ G_{|s\rangle\langle s| \otimes {\bf b}},\; G_{|s\rangle\langle s| \otimes i{\bf b}} : s=1,2,...,d \} \\ \nonumber && \cup \{ G_{|s\rangle\langle s| \otimes {\bf b}^\dagger},\; G_{|s\rangle\langle s| \otimes i{\bf b}^\dagger} : s=1,2,...,d \} \\ \nonumber && \cup \{ (|s\rangle\langle s| \otimes {\bf I}) \rho (|j\rangle\langle j| \otimes {\bf I}) + (|j\rangle\langle j| \otimes {\bf I}) \rho (|s\rangle\langle s| \otimes {\bf I}) \;\; : s,j=1,2,...,d \;,\;\; j<s \} \\ \nonumber && \cup \{ i(|s\rangle\langle s| \otimes {\bf I}) \rho (|j\rangle\langle j| \otimes {\bf I}) - i(|j\rangle\langle j| \otimes {\bf I}) \rho (|s\rangle\langle s| \otimes {\bf I}) \;\; : s,j=1,2,...,d \;,\;\; j<s \} \\ \nonumber && \cup \{ (|s\rangle\langle s| \otimes {\bf b}) \rho (|j\rangle\langle j| \otimes {\bf I}) + (|j\rangle\langle j| \otimes {\bf I}) \rho (|s\rangle\langle s| \otimes {\bf b}^\dagger) \;\; : s,j=1,2,...,d \;,\;\; j \neq s \} \\ \nonumber && \cup \{ i(|s\rangle\langle s| \otimes {\bf b}) \rho (|j\rangle\langle j| \otimes {\bf I}) - i(|j\rangle\langle j| \otimes {\bf I}) \rho (|s\rangle\langle s| \otimes {\bf b}^\dagger) \;\; : s,j=1,2,...,d \;,\;\; j \neq s \} \; .\\\end{eqnarray} \]

Proof: We must find the smallest algebra \( \tilde{\mathfrak{G}}_F\) generated by the vector fields \( G_\bf{{ I} \otimes \bf{ b}}\) , \( G_\bf{{ I} \otimes i\bf{ b}}\) (measurements) and \( G_\bf{{ I} \otimes \bf{ b}^\dagger}\) , \( G_\bf{{ I} \otimes i\bf{ b}^\dagger}\) (independent linear combination of measurement and control vector fields), and commuting with \( F_\bf{{ I} \otimes \bf{ b}} + \eta D_\bf{{ I} \otimes \bf{ b}}\) as well as with the coupling Hamiltonian.

The first three lines of (24) are obtained similarly to the proof of Prop.9. Note that we have dropped the vector fields of the form \( G_{|s\rangle\langle s| \otimes i\bf{ I}}\) in the first line, because they are included in the set described in the fifth line. The new contributions are obtained as follows.

  • -

    Commuting \( G_{Q_A^s \otimes \delta\bf{ b}^\dagger}\) with \( F_\bf{{ I} \otimes \bf{ b}} + \eta D_\bf{{ I} \otimes \bf{ b}}\) yields a vector field of the form

    \[ (Q_A^s\otimes {\bf I}) \rho ({\bf I} \otimes \delta{\bf b}^\dagger) - \text{Trace}((Q_A^s\otimes {\bf I}) \rho ({\bf I} \otimes \delta{\bf b}^\dagger)) \;\; + \text{\emph{hermit.conj.}} \; . \]

    Taking a linear combination with previously constructed vector fields, we can rewrite it as (dropping the \( \bf{ I}\) symbols to avoid cluttered notation):

    \[ Q_A^s \rho \delta{\bf b}^\dagger + \delta^* {\bf b} \rho Q_A^s - (Q_A^s \otimes \delta^*{\bf b}) \rho -\rho (Q_A^s \otimes \delta {\bf b}^\dagger) \; . \]
  • -

    Further repeated commutations with the third line of (24), the Hamiltonian coupling, and \( F_\bf{{ I} \otimes \bf{ b}} + \eta D_\bf{{ I} \otimes \bf{ b}}\) yields all the vector fields of the form

    \[ \begin{eqnarray*} && Q_A^m \rho Q_A^k + Q_A^k \rho Q_A^m - Q_A^{m+k} \rho - \rho Q_A^{m+k}\\ &\text{ or } & i (Q_A^m \rho Q_A^k - Q_A^k \rho Q_A^m)\\ &\text{ or } & {\bf b} Q_A^m \rho Q_A^k + Q_A^k \rho Q_A^m {\bf b}^\dagger - {\bf b} Q_A^{m+k} \rho - \rho Q_A^{m+k} {\bf b}^\dagger \; , \end{eqnarray*} \]

    as well as the ones obtained by replacing \( \bf{ b}\) by \( i\bf{ b}\) .

  • - One can now check that these vector fields form a closed algebra under mutual commutation, and under further commutation with the coupling Hamiltonian or with \( F+\eta D\) .

The statement then follows by matching the basis involving operators \( Q_A^k\) to the basis involving eigenstate projectors \( |s\rangle\langle s|\) . \( \square\)

Proposition 10 is helpful towards characterizing the manifolds under the form (7). In fact, this provides a fully general representation of the link between input and output signals of the system (13) via \( 3 d^2 + 2 d -1\) dynamic parameters. An Ansatz using the Wigner function of the cavity, as in Section 3.2, leads to the following result. The expressions may look somewhat long, but remember that they analytically and exactly describe the solution of a composite quantum system. Simplified expressions are provided below (special case without control, and asymptotic long-times analysis).

Proposition 11

The quantum SDE (13), for a general initial condition, admits the explicit solution:

\[ \rho_t = \sum_{j,k=1}^{d} |j\rangle\langle k| \otimes \rho_{t,(j,k)} \; , \]

where each \( \rho_{t,(j,k)}\) is an operator on the cavity Hilbert space evolving as follows. Denote \( \omega_k = \chi (Q_A)_{k,k}\) and \( \omega_{j,k}=\chi((Q_A)_{j,j}-(Q_A)_{k,k})\) .

The diagonal-block operators \( \rho_{t,(k,k)}\) correspond to the unnormalized Wigner representation:

\[ \mathcal{W}^{ \{\rho_{t,(k,k)}\} }(\,x\;,\;p\,) = \mu_{t,k} \, \tfrac{1}{\Pi\, s_t}\; \iint \mathcal{W}^{\{\rho_{0,(k,k)}/\mu_{0,k}\}}(x_0,p_0)\, K_{k,t}(x,x_0,p,p_0) \, dx_0\, dp_0 \; , \]
\[ \begin{eqnarray*} K_{k,t}(...) &=& \exp{\left( \frac{-\left\Vert \left(\begin{array}{c} x-\xi_{t,k} \\ p-\pi_{t,k} \end{array}\right)- a_t R_{kt} \left(\begin{array}{c} x_0 \\ p_0 \end{array}\right) \right\Vert^2}{s_t} + d_t \left\Vert \begin{array}{c} x_0 \\ p_0 \end{array} \right\Vert^2 + \left(\begin{array}{c} \theta_{t,k} \\ \zeta_{t,k} \end{array}\right)^T R_{kt} \left(\begin{array}{c} x_0 \\ p_0 \end{array}\right) \right)}\;\; , \end{eqnarray*} \]

where we have introduced the rotation matrix

\[ R_{kt} = \left(\begin{array}{cc} \cos(\omega_k t) & -\sin(\omega_k t) \\ \sin(\omega_k t) & \cos(\omega_k t) \end{array}\right) \; . \]

The deterministic parameters involved in this expression evolve as:

\[ \begin{eqnarray*} a_t &=& \frac{2 e^{-t}}{(2-\eta) + \eta\, e^{-2 t}} \\ s_t &=& \tfrac{1}{2} \, (1-a_t e^{-t})\\ d_{t} &=& a_t \, \eta \, (e^{-t}-e^{t})\\ \frac{d}{dt}\left(\begin{array}{c} z_{t,k} \\ y_{t,k} \end{array}\right) &=& \, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right) - \left(\begin{array}{c} z_{t,k} \\ y_{t,k} \end{array}\right) + \omega_k \left(\begin{array}{cc} -y_{t,k} \\ z_{t,k} \end{array}\right) ~ , ~ \left(\begin{array}{c} z_{0,k} \\ y_{0,k} \end{array}\right) = 0 \; , \\ && \text{characterizing } \left(\begin{array}{c} \theta_{t,k} \\ \zeta_{t,k} \end{array}\right) = 4\, e^t \, \left(\begin{array}{c} z_{t,k}- \xi_{t,k} \\ y_{t,k} - \pi_{t,k} \end{array}\right) \; . \end{eqnarray*} \]

Thus the \( \rho_{t,(k,k)}\) depend on the measurement results only through the parameters:

\[ \begin{eqnarray} \nonumber d\left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right) & = & \frac{-a_t e^{-t}\sqrt{\eta}}{2}\, \left( \begin{array}{c} dy_{t,1}-2 \sqrt{\eta}\xi_{t,k}\, dt \\ dy_{t,2} -2 \sqrt{\eta} \pi_{t,k} \, dt \end{array} \right) \\ && ~ + \left( \, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right) - \left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right) + \omega_k \left(\begin{array}{cc} -\pi_{t,k} \\ \xi_{t,k} \end{array}\right) \, \right) dt \; , \end{eqnarray} \]

(25)

\[ \begin{eqnarray} d(\mu_{t,k}) & = & -2 \sqrt{\eta} \mu_{t,k} \left( \left(\begin{array}{c} \bar{x}_t \\ \bar{p}_t \end{array}\right) -\left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right) \right)^T \left(\begin{array}{c} dy_{t,1}-2\sqrt{\eta}\bar{x}_t dt \\ dy_{t,2}-2\sqrt{\eta}\bar{p}_t dt \end{array}\right) \end{eqnarray} \]

(26)

\[ \begin{eqnarray} && \text{ with } 2\bar{x}_t = \text{Trace}(({\bf b} + {\bf b}^\dagger)\, \rho_t) \;\;\; \text{ and } 2\bar{p}_t = \text{Trace}(i({\bf b} - {\bf b}^\dagger)\, \rho_t) \; . \\\end{eqnarray} \]

These variables are initialized with \( \xi_{0,k} = \pi_{0,k}=0\) , while \( \mu_{0,k} = \text{Trace}(\rho_{0,(k,k)})\) . The sum of the \( \mu_{t,k}\) is fixed by normalization, leading to \( 3d-1\) independent stochastic variables for these block-diagonal components, and \( 2d\) additional variables which depend on the control inputs.

The off-diagonal-block operators

\[ \rho_{t,(j,k)} = e^{-i \tfrac{\omega_{k}+\omega_j}{2}\, {\bf N}t}\, \tilde{\rho}_{t,(j,k)}\, e^{i\tfrac{\omega_{k}+\omega_j}{2}\, {\bf N}t} \, , \]

with \( \bf{ N} = \bf{ b}^\dagger \bf{ b}\) and \( j \neq k\) , involve \( \tilde{\rho}_{t,(j,k)}\) associated to the unnormalized Wigner function:

\[ \mathcal{W}^{\{\tilde{\rho}_{t,(j,k)}\}}(x,p) = \tfrac{\mu_{t,(j,k)}}{\Pi\, s_{t,(j,k)}}\; \int \int \mathcal{W}^{\{\tilde{\rho}_{0,(j,k)}/ \mu_{0,(j,k)}\}}(x_0,p_0)\, K_{(j,k),x,t}(x,x_0)\, K_{(j,k),p,t}(p,p_0) \, dx_0\, dp_0 \; , \]
\[ \begin{eqnarray*} K_{(j,k),x,t}(x,x_0) &=& \exp\left( \frac{-(x-x_0 a_{t,(j,k)} - \xi_{t,(j,k)})^2}{s_{t,(j,k)}} + (d_{t,(j,k)} x_0^2+\theta_{t,(j,k)}x_0) \right)\;\; , \\ K_{(j,k),p,t}(p,p_0) &=& \exp\left( \frac{-(p-p_0 a_{t,(j,k)} - \pi_{t,(j,k)})^2}{s_{t,(j,k)}} + (d_{t,(j,k)} p_0^2+\zeta_{t,(j,k)}p_0) \right)\;\;. \end{eqnarray*} \]

The parameters in these expressions belong to \( \mathbb{C}\) . The deterministic parameters involved in these expressions, and not controllable by the inputs \( (u_t,v_t)\) independently of the diagonal blocks, evolve as follows:

\[ \begin{eqnarray*} a_{t,(j,k)} &=& \frac{(2+i\omega_{j,k}) e^{-(1+i\tfrac{\omega_{j,k}}{2})t}}{(2-\eta+i\tfrac{\omega_{j,k}}{2}) + (\eta+i\tfrac{\omega_{j,k}}{2})\, e^{-(2+i\omega_{j,k}) t}} \\ s_{t,(j,k)} &=& \tfrac{1}{2} \, (1-a_{t,(j,k)} e^{-(1+i\tfrac{\omega_{j,k}}{2})t})\\ d_{t,(j,k)} &=& a_{t,(j,k)} \, \frac{2\eta+i\omega_{j,k}}{2+i\omega_{j,k}} \, (e^{-(1+i\tfrac{\omega_{j,k}}{2})t}-e^{(1+i\tfrac{\omega_{j,k}}{2})t})\\ \left(\begin{array}{c} z_{t,(j,k)} \\ y_{t,(j,k)} \end{array}\right) &=& \tfrac{1}{2} \left(\; \left(\begin{array}{cc} 1 & i \\ - i & 1 \end{array}\right) R_{\tfrac{\omega_{j,k}}{2}\,t} \left(\begin{array}{c} z_{t,k} \\ y_{t,k} \end{array}\right) + \left(\begin{array}{cc} 1 & -i \\ i & 1 \end{array}\right) R_{\tfrac{-\omega_{j,k}}{2}\,t} \left(\begin{array}{c} z_{t,j} \\ y_{t,j} \end{array}\right) \;\right) \\ &&\text{characterizing } \left(\begin{array}{c} \theta_{t,(j,k)} \\ \zeta_{t,(j,k)} \end{array}\right) = 4 e^{(1+i\tfrac{\omega_{j,k}}{2})t} \, \left(\begin{array}{c} z_{t,(j,k)}- \xi_{t,(j,k)} \\ y_{t,(j,k)} - \pi_{t,(j,k)} \end{array}\right) \; . \end{eqnarray*} \]

The \( (3d-1)(d-1)\) deterministic variables, which can be driven to independent values by the input signals \( (u_t,v_t)\) , evolve as follows:

\[ \begin{eqnarray*} \tfrac{d}{dt}\left(\begin{array}{c} X_{t,(j,k)} \\ P_{t,(j,k)} \end{array}\right) &=& \left(\frac{1}{a_{t,(j,k)}} - \frac{e^{-i\tfrac{\omega_{j,k}}{2}\,t}}{a_t}\right)\, R_{\tfrac{\omega_j+\omega_k}{2}t}\, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right) ~ \text{ with } \left(\begin{array}{c} X_{0,(j,k)} \\ P_{0,(j,k)} \end{array}\right) =0 \\ && \text{characterizing } \;\; \left(\begin{array}{c} \xi_{t,(j,k)} \\ \pi_{t,(j,k)} \end{array}\right) \;=\; a_{t,(j,k)} \, \left(\begin{array}{c} X_{t,(j,k)} \\ P_{t,(j,k)} \end{array}\right) \\ && + \frac{a_{t,(j,k)}}{2 a_t}\, e^{-i\tfrac{\omega_{j,k}}{2}\,t}\, { \left(\; \left(\begin{array}{cc} 1 & i \\ - i & 1 \end{array}\right) R_{\tfrac{\omega_{j,k}}{2}\,t} \left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right) + \left(\begin{array}{cc} 1 & -i \\ i & 1 \end{array}\right) R_{\tfrac{-\omega_{j,k}}{2}\,t} \left(\begin{array}{c} \xi_{t,j} \\ \pi_{t,j} \end{array}\right) \;\right)} \; \\ \tfrac{d}{dt} c_{t,(j,k)} &=& \Re\left((\eta+i\tfrac{\omega_{jk}}{2})\,a_{t,(j,k)}\,e^{-(1+i\tfrac{\omega_{j,k}}{2})t}\right) - \eta\, a_t\,e^{-t} \\ && + 4 \Re\left(\, e^{(1+i\tfrac{\omega_{j,k}}{2})t} \left(\begin{array}{c} X_{t,(j,k)} \\ P_{t,(j,k)} \end{array}\right)^T \, R_{\tfrac{\omega_k+\omega_j}{2}t} \, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right)\, \right) \\ && \text{characterizing } \;\; \log\left(\frac{|\mu_{t,(j,k)}|}{\sqrt{\mu_{t,j}\mu_{t,k}}}\right) \;=\; c_{t,(j,k)} -\Re\left(\,\frac{2 e^{(1+i\tfrac{\omega_{j,k}}{2})t}}{a_{t,(j,k)}} (\xi_{t,(j,k)}^2 + \pi_{t,(j,k)}^2)\,\right) \\ && ~~ ~~ ~~ ~~ ~~ ~~ + \frac{e^t}{a_t} (\xi_{t,k}^2+\pi_{t,k}^2+\xi_{t,j}^2+\pi_{t,j}^2) \\ \tfrac{d}{dt} q_{t,(j,k,\ell)} &=& Q_{t,(j,k)} + Q_{t,(k,\ell)} + Q_{t,(\ell,j)} \\ && \text{where } \;\; Q_{t,(j,k)}\;=\; \Im\left((\eta+i\tfrac{\omega_{j,k}}{2})a_{t,(j,k)}\,e^{-(1+i\tfrac{\omega_{j,k}}{2})t}\right)\\ && ~~ ~~ ~~ ~~ ~~ +4 \Im\left(\, e^{(1+i\tfrac{\omega_{j,k}}{2})t} \left(\begin{array}{c} X_{t,(j,k)} \\ P_{t,(j,k)} \end{array}\right)^T \, R_{\tfrac{\omega_k+\omega_j}{2}t} \, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right)\, \right) \;\; , \end{eqnarray*} \]

characterizing \( \; \text{phase}(\mu_{t,(j,k)}\mu_{t,(k,\ell)}\mu_{t,(\ell,j)}) =\)

\[ \begin{eqnarray*} && q_{t,(j,k,\ell)} - 2 \Im\left( \frac{e^{(1+i\tfrac{\omega_{j,k}}{2})t}}{a_{t,(j,k)}}(\xi_{t,(j,k)}^2 + \pi_{t,(j,k)}^2) \right) \\ && - 2 \Im\left( \frac{e^{(1+i\tfrac{\omega_{k,\ell}}{2})t}}{a_{t,(k,\ell)}}(\xi_{t,(k,\ell)}^2 + \pi_{t,(k,\ell)}^2) \right) - 2 \Im\left( \frac{e^{(1+i\tfrac{\omega_{\ell,j}}{2})t}}{a_{t,(\ell,j)}}(\xi_{t,(\ell,j)}^2 + \pi_{t,(\ell,j)}^2) \right) \; . \end{eqnarray*} \]

The last variables are initialized from \( \mu_{0,(j,k)} = \text{Trace}(\rho_{0,(j,k)})\) . The measurement realizations add new degrees of freedom to the off-diagonal blocks, only through:

\[ \begin{eqnarray*} \tfrac{d}{dt} \delta_{t,(j,k)} &=& Q_{t,(j,k)} +\frac{2\,e^t}{a_t}\left( \left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right)^T R_{\omega_k t} - \left(\begin{array}{c} \xi_{t,j} \\ \pi_{t,j} \end{array}\right)^T R_{\omega_j t}\right) \, \left(\begin{array}{c} u_t \\ v_t \end{array}\right) \\ && \text{characterizing } \;\; \text{phase}(\mu_{t,(j,k)}) \;=\; \delta_{t,(j,k)} - 2 \Im\left( \frac{e^{(1+i\tfrac{\omega_{j,k}}{2})t}}{a_{t,(j,k)}}(\xi_{t,(j,k)}^2 + \pi_{t,(j,k)}^2) \right) \; . \end{eqnarray*} \]

The latter are linked through the deterministic variables \( q_{t,(j,k,\ell)}\) , such that they can move only in a subspace of dimension \( d-1\) as a function of the measurement realizations.

Proof: From (13), each component \( \langle k| \rho |j\rangle\) of the state, with \( j,k\) two qudit levels, evolves independently --- up to the common variables \( \bar{x}_t\) and \( \bar{p}_t\) . The latter only depend on \( \{\langle k| \rho |k\rangle : k=1,2,..., d\}\) , so these diagonal blocks undergo autonomous dynamics. Furthermore, the dependence of \( d \langle k| \rho |j\rangle\) on \( \bar{x}_t\) and \( \bar{p}_t\) multiplies \( \langle k| \rho |j\rangle\) itself, so it looks mainly as a normalization. It is important to note the detuning though: for each level \( k\) , the output and input analogous to Prop.3 would be in a different rotating frame. In a Rotating Wave Approximation (RWA), we would say that each qudit level is associated to a cavity state driven by separate inputs and outputs, corresponding to a component at the resonance frequency only. This has motivated the form of the solution, analogous to one cavity per qudit level, with a Prop.3 type solution except each level gets its own variables and the normalization of each cavity state is now explicitly computed.

For the diagonal blocks \( \langle k| \rho |k\rangle\) , the equations to be solved in Wigner representation are exactly the same as for Proposition 3. We just have to rotate input and output into the correct frame. This time, we explicitly compute the equation for the normalization constants, and we find how they depend on the measurement signals. Note that the deterministic parameters do not depend on \( k\) .

Since we have assumed \( n_{th}=0\) , the component \( \theta_k\) is deterministically linked to \( \xi_k\) as in Prop.3, but it cannot be explicitly integrated since this link depends on the control inputs in a \( k\) -dependent way. Also, for \( u_t,v_t\) nonzero, a given state of the cavity cannot be linked uniquely to a normalization constant for the corresponding qudit level: there is a memory effect, implying a separate dependence on the output signals, so the \( \mu_k\) must be integrated separately.

For the off-diagonal blocks \( \langle j| \rho |k\rangle\) with \( j\neq k\) , the corresponding cavity density operator component is non-hermitian and cannot be considered anymore as an unnormalized cavity state. We can nevertheless write the Wigner representation, accepting \( \mathcal{W}\) to be complex rather than real. The algebraic criterion, by giving the number of independent parameters that depend on \( dy_1,dy_2,u_t\) and \( v_t\) as well as the associated vector fields, has been an invaluable tool towards guessing which representation could work. The proof then comes down, to a big extent, to identifying the resulting equations and solving them exactly like for the cavity alone. We consider each off-diagonal block independent in a first approach, planning to look for remaining dependencies later.

The stochastic partial differential equation followed by the Wigner representation of \( \langle j| \rho |k\rangle\) contains an additional contribution:

\[ \begin{multline*} d\rho_{t,(j,k)} = ... - i \tfrac{\omega_j-\omega_k}{2}(\,{\bf b}^\dagger {\bf b} \rho_{t,(j,k)} + \rho_{t,(j,k)}{\bf b}^\dagger {\bf b}\, ) dt + .... \\ \leftrightarrow d\mathcal{W}^{\{\rho_{t,(j,k)} \}} = ... -i(\omega_j-\omega_k) \, \left( x^2+p^2 - \tfrac{1}{2} - \tfrac{1}{16}(\tfrac{\partial^2}{\partial x^2} +\tfrac{\partial^2}{\partial p^2} ) \right) \, \mathcal{W} \, dt + ... \;\; . \end{multline*} \]

The equation is still separable in \( x\) and \( p\) , so we try the same Gaussian representation as for the cavity alone, but now allowing complex parameters. We also assume a priori that all the parameters could depend on the index \( (j,k)\) .

From there, we proceed like for the other cases. First, we see that the partial stochastic differential equation contains no term in \( x^2 dw_{t,1}\) and therefore \( s_{t,(j,k)}\) is deterministic. The corresponding ODE is:

\[ \frac{ds_{t,(j,k)}}{dt} + 2 \eta (s_{t,(j,k)}-\tfrac{1}{2})^2 = -2 s_{t,(j,k)} + 1 - i (\omega_j-\omega_k)(s_{t,(j,k)}^2 - \tfrac{1}{4})\, . \]

The equation can again be solved as a Ricatti form, it just depends, indeed, on \( (j,k)\) . Going on like for the single cavity, yields the deterministic solutions for \( a_{t,(j,k)}\) and \( d_{t(j,k)}\) . Those do not depend on outputs nor inputs. The equations for the remaining parameters \( \xi_{t,(j,k)}, \theta_{t,(j,k)}\) and \( \mu_{t,(j,k)}\) do involve inputs and outputs. Note that \( \mu_{t,(j,k)}\) is split between \( x\) and \( p\) contributions, the overall equation is easily obtained by analogy.

The off-diagonal parameters computed in this way are not all independent. Indeed, from Proposition 10, the overall solution should involve \( 3d^2+2d-1\) true degrees of freedom depending on outputs or inputs, among which \( 4d-2\) can depend on the outputs. The diagonal blocks already involve \( 5d-1\) degrees of freedom, among which \( \xi_k,\pi_k,\mu_k\) are \( 3d-1\) variables depending on outputs, while \( z_{k},y_{k}\) depend on the inputs. Thus there should remain \( 3d(d-1)\) independent variables, among which only \( d-1\) can be driven independently by the outputs. Instead, in total, our complex parameterization involves \( 5d(d-1)\) real degrees of freedom through the \( (\xi,\pi,\mu,\theta,\zeta)_{(j,k)}\) .

The parameters \( (\theta,\zeta)_{(j,k)}\) can be written as functions of \( (\xi,\pi)\) and of deterministic variables \( z_{(j,k)},y_{(j,k)}\) , like for the diagonal components. We can rotate back the vector \( (z,y)\) to a common rotating frame, for indices \( (k,k)\) , \( (j,j)\) and \( (j,k)\) . Then we separate the real and imaginary parts of the \( (j,k)\) components, and we observe the resulting dynamics in \( \mathbb{R}^8\) : the vector fields span a 4-dimensional linear subspace, such that real and imaginary components of \( z_{(j,k)},y_{(j,k)}\) are just static linear functions of \( (z_k,y_k)\) and \( (z_j,y_j)\) , in any common rotating frame. This suppresses \( 2d(d-1)\) parameters and indeed leaves \( 3d(d-1)\) independent ones, among which only \( d-1\) may depend on the output realization.

For the \( (\xi,\pi)_{(j,k)}\) , we can repeat a procedure similar to the \( (z,y)_{(j,k)}\) , linking real and imaginary parts to \( (j,j)\) and \( (k,k)\) components in rotating frame. The control vector field does not drop out of these equations, yielding thus \( 2d(d-1)\) parameters which can be driven independently by the control vector fields (only).

We are thus left with the \( \mu_{t,(j,k)}\) , among which \( d-1\) degrees of freedom can depend on measurement realizations, while all the remaining ones are provided by the input signals. We must thus find a variable where the noise term cancels, and the rest “looks nice”. From the SDEs describing \( \xi_{t,(j,k)},\pi_{t,(j,k)}\) and \( \mu_{t,(j,k)}\) , we consider the variables:

\[ \tilde{m}_{(j,k)} := \log(\mu_{j,k}) - \frac{\xi_{t,(j,k)}^2+\pi_{t,(j,k)}^2}{s_{t,(j,k)}-1/2} \; , \]

Indeed, in the corresponding SDEs, the noise term becomes independent of the indices \( j,k\) , namely:

\[ \begin{eqnarray*} d\tilde{m}_{t,(j,k)} &=& -2\sqrt{\eta} \left(\begin{array}{c} \bar{x}_t \\ \bar{p}_t \end{array}\right)^T \left(\begin{array}{c} dy_{t,1} \\ dy_{t,2} \end{array}\right) - (2 \eta + i (\omega_j-\omega_k))(s_{t,(j,k)}-\tfrac{1}{2})\, dt \\ && - \tfrac{2}{s_{t,(j,k)}-\tfrac{1}{2}}\left(\begin{array}{c} \xi_{t,(j,k)} \\ \pi_{t,(j,k)} \end{array}\right)^T \, R_{\tfrac{\omega_j+\omega_k}{2}t} \, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right) \, dt \; . \end{eqnarray*} \]

Thus, taking linear combinations of such variables, with linear coefficients summing to zero, allows to cancel the noise term. In general, there would remain a dependence on \( \xi,\pi\) , through which the system might diffuse in many directions, like the rolling wheel. But we have just established the interdependence of the \( (\xi,\pi)_{(j,k)}\) too, up to control signals. Knowing this, we consider just

\[ m_{(j,k)} = \tilde{m}_{(j,k)}- \tfrac{1}{2}(\tilde{m}_{(j,j)}+\tilde{m}_{(k,k)})\; , \]

i.e. the coherence compared to its associated diagonals. Using the interdependence of the \( \xi,\pi\) , the corresponding differential equation writes:

\[ \begin{eqnarray*} dm_{t,(j,k)}&=& 2\eta(s_t-\tfrac{1}{2})\, dt - (2 \eta + i (\omega_j-\omega_k))(s_{t,(j,k)}-\tfrac{1}{2})\, dt\\ && + 4 e^{(1+i\tfrac{\omega_j-\omega_k}{2})t} \, \left(\begin{array}{c} X_{t,(j,k)} \\ P_{t,(j,k)} \end{array}\right)^T \, R_{\tfrac{\omega_j+\omega_k}{2}t} \, \left(\begin{array}{c} v_t \\ -u_t \end{array}\right) \, dt \\ && + \frac{i}{s_t-\tfrac{1}{2}} \left(\begin{array}{c} \xi_{t,j} \\ \pi_{t,j} \end{array}\right)^T \, R_{\omega_j t} \, \left(\begin{array}{c} u_t \\ v_t \end{array}\right) \, dt - \frac{i}{s_t-\tfrac{1}{2}} \left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right)^T \, R_{\omega_k t} \, \left(\begin{array}{c} u_t \\ v_t \end{array}\right) \, dt \; . \end{eqnarray*} \]

In the real part of \( dm_{(j,k)}\) , all the variables \( \xi,\pi\) disappear and we obtain an equation involving deterministic parameters and the input signals \( u_t,v_t\) . In the imaginary part of \( m_{(j,k)}\) , a dependence on \( \xi_k,\pi_k\) and \( \xi_j,\pi_k\) remains. This is expected, since \( d-1\) degrees of freedom can still be driven by measurement realizations. The reduction from \( d(d-1)/2\) to \( d-1\) is made by noticing how any \( \xi,\pi\) again disappear in linear combinations \( m_{(j,k)} + m_{(k,l)} + m_{(l,j)}\) .

With this we have treated all the parameters. Note how the algebraic criterion has been crucial in order to identify when interdependencies remained, and when we can stop because no further reduction is possible for a general initial state and general input signals. \( \square\)

Proposition 12

For \( v_t=u_t=0\) , i.e. in absence of drives on the cavity, the solution of Proposition 11 simplifies as follows:

\[ \begin{array}{rlrl} \theta_{t,k} &=\; -4\, e^{t}\,\xi_{t,k} \;\; , ~ & \zeta_{t,k} &=\; -4\, e^{t}\, \pi_{t,k} \;\; ,\\ \theta_{t,(j,k)} &=\; -4\, e^{(1+i\tfrac{\omega_{j,k}}{2})\,t} \xi_{t,(j,k)} \;\; , ~ & \zeta_{t,(j,k)} &=\; -4\, e^{(1+i\tfrac{\omega_{j,k}}{2})\,t} \pi_{t,(j,k)} \;\; ; \end{array} \]
\[ \left(\begin{array}{c} \xi_{t,(j,k)} \\ \pi_{t,(j,k)} \end{array}\right) \;=\; \frac{a_{t,(j,k)}}{2 a_t}\, e^{-i\tfrac{\omega_{j,k}}{2}\,t}\, \left(\; \left(\begin{array}{cc} 1 & i \\ - i & 1 \end{array}\right) R_{\tfrac{\omega_{j,k}}{2}\,t} \left(\begin{array}{c} \xi_{t,k} \\ \pi_{t,k} \end{array}\right) + \left(\begin{array}{cc} 1 & -i \\ i & 1 \end{array}\right) R_{\tfrac{-\omega_{j,k}}{2}\,t} \left(\begin{array}{c} \xi_{t,j} \\ \pi_{t,j} \end{array}\right) \;\right) \; ; \]
\[ \begin{align*} \mu_{t,k} &= \mu_{0,k}\, a_t \, \exp\left( t+ \frac{\xi_{t,k}^2+\pi_{t,k}^2}{s_t-1/2}\right) \, \nu_t \; \, ,\\ \mu_{t,(j,k)} &= \mu_{0,(j,k)}\, a_{t,(j,k)} \, \exp\left( (1+\tfrac{i\omega_{j,k}}{2})\,t + \frac{\xi_{t,(j,k)}^2+\pi_{t,(j,k)}^2}{s_{t,(j,k)}-1/2}\right) \, \nu_t \; \, , \end{align*} \]

with \( \nu_t\) a common normalization constant.

Proof: According to the algebraic criterion, in the diagonal components already, the normalization constants \( \mu_k\) must become deterministically linked to \( \xi_k,\pi_k\) . Like for the interdependence of the \( \mu_{(j,k)}\) in the above proof, the variable

\[ \frac{\xi_{t,k}^2+\pi_{t,k}^2}{s_t-1/2} - \frac{\xi_{t,j}^2+\pi_{t,j}^2}{s_t-1/2} - \log(\mu_{t,k}/\mu_{t,j}) \]

appears like a good candidate. One then checks that indeed, it undergoes an autonomous deterministic equation, provided \( u=v=0\) . This evolution of \( \mu_{t,k}/\mu_{t,j}\) is compatible with introducing a common multiplicative constant and stating the explicit expression of the \( \mu_k\) as done in the statement.

In the off-diagonal parameterization, a similar treatment holds for the \( \mu_{t,(j,k)}\) when \( u=v=0\) . In particular, this fixes the phase of each \( \mu_{t,(j,k)}\) as a deterministic function of the \( \xi_{t,(j,k)}\) and \( \pi_{t,(j,k)}\) . For the other variables, \( z_{t,(j,k)},y_{t,(j,k)},\xi_{t,(j,k)},\pi_{t,(j,k)}\) which would be driven independently of the diagonal blocks only through control inputs \( u_t,v_t\) , the degree of freedom obviously disappears once \( u_t=v_t=0\) . \( \square\)

The result of Proposition 12 thus indicates that, for \( u_t=v_t=0\) , once the \( 2d\) values at time \( t\) of the “mean position parameters” \( \xi_{t,k}\) and \( \pi_{t,k}\) in the Green function are known, this defines the full state completely. In presence of control, the situation as described in Proposition 11 is more complicated. In particular: (i) the diagonal normalization constants \( \mu_{t,k}\) are not deterministically linked anymore to the conditional cavity state; and (ii) the global angles of each conditional cavity state, expressed through the off-diagonal normalization constants \( \mu_{t,(j,k)}\) , are not deterministically linked to the rest of the system. All the other variables are essentially deterministically linked to \( \xi_{t,k}\) and \( \pi_{t,k}\) , but some of them can be driven to independent values by the \( (u_t,v_t)\) . This can be understood with the following standard approach: qudit level \( |s\rangle\) shifts the cavity frequency by \( \chi {Q_A}_{s,s}\) , and driving the cavity on resonance with this shift would mainly, independently, drive the part of the state conditioned on qudit level \( |s\rangle\) . A few further remarks are in order.

  • For a general initial state, the \( \mu_{t,(j,k)}\) or \( \mu_{t,k}\) , are not necessarily equal to the trace of \( \rho_{t,(j,k)}\) for \( t>0\) . The full normalization indeed involves the integral with \( \mathcal{W}^{\{\tilde{\rho}_{0,(j,k)}\}}(x_0,p_0)\) . Although some interesting features already appear — e.g. \( \mu_k\) is less subject to Wiener noise if its \( \xi_{t,k},\pi_{t,k}\) match well with \( \bar{x}_t,\bar{p}_t\) — more conclusive treatments have to assume a particular type of initial state for the joint system, since the general case cannot be further reduced. In particular, the normalization is maybe not just \( \sum_k \mu_{t,k} = 1\) .
  • If some qudit level is initially not populated, i.e. \( \mu_{0,k}=0\) for some \( k \in \{1,2,...,d\}\) , then \( \mu_{t,k}=0\) for all times and the corresponding \( \rho_{t,(j,k)}\) can be dropped.
  • Interdependence of the phases of the \( \mu_{t,(j,k)}\) is an expected feature. Indeed, starting with an arbitrary positive hermitian matrix \( \rho\) , if the off-diagonals could pick up independent complex phases, then the state would not necessarily remain positive.

Finally, in order to gain more concrete insight on the meaning of Proposition 11, we consider its result as \( t \rightarrow +\infty\) . We first observe that

\[ \begin{eqnarray*} a_0=1 \rightarrow a_{+\infty}=0 &\;\; \text{ and } \;\; & s_0=0 \rightarrow s_{+\infty}=1/2 \end{eqnarray*} \]

at a unit exponential rate. This indicates that, up to normalization, \( \mathcal{W}^{ \{\rho_{t,(k,k)}\} }(x,p)\) becomes independent of the initial condition. It exponentially converges towards the Wigner function of the vacuum. This vacuum is displaced by the shift in the Wigner arguments in the diagonal-block, leading to a coherent state \( |\alpha\rangle\) with \( \alpha_k = \xi_{t,k} + i \pi_{t,k} \in \mathbb{C}\) .

In the SDE (25) governing \( \xi_{t,k}+i\pi_{t,k}\) , the dependence on measurement outputs also decreases exponentially, such that asymptotically they follow the ordinary differential equation:

\[ \begin{eqnarray*} \tfrac{d}{dt} \, \alpha_{t,k} = (v_t-i\,u_t) + i\, \omega_k \alpha_{t,k} \, - \alpha_{t,k} \; . \end{eqnarray*} \]

This is the standard level-dependent evolution of a coherent state in a “readout-cavity” to be probed, see e.g. [59].

The normalization, reflecting respective qudit populations, is then given by:

\[ \begin{eqnarray*} \tilde{\mu}_k & = & \mu_{t,k} \iint \mathcal{W}^{\{\rho_{0,(k,k)}\}}(x_0,p_0) \; \exp\left( \tfrac{-2\eta}{2-\eta}\left\Vert\begin{array}{c} x_0 \\ p_0 \end{array} \right\Vert^2 + \left(\begin{array}{c} \theta_{t,k} \\ \zeta_{t,k} \end{array}\right)^T R_k \left(\begin{array}{c} x_0 \\ p_0 \end{array}\right)\,\right) \, dx_0 dp_0 \; . \end{eqnarray*} \]

Recalling from Section 3.2.1 that

\[ d\left( \begin{array}{c} \theta_{t,k} \\ \zeta_{t,k} \end{array} \right) = 2 \sqrt{\eta} a_t \left( \begin{array}{c} dw_{t,1} \\ dw_{t,2} \end{array} \right) + 4 \eta a_t \left( \begin{array}{c} \bar{x}_t - \xi_{t,k} \\ \bar{p}_t - \pi_{t,k} \end{array} \right) \, dt + \omega_k \left( \begin{array}{c} -\zeta_{t,k} \\ \theta_{t,k} \end{array} \right) \, dt \]

and considering (again) that \( \bar{x},\bar{p},\xi_k,\pi_k\) would remain bounded with high probability, we see that \( \tfrac{\tilde{\mu}_k}{\mu_k}\) asymptotically converges towards a time-independent value for each \( k\) . We then have in fact, asymptotically:

\[ \begin{eqnarray} d\tilde{\mu}_{t,k} &=& 2 \sqrt{\eta} \left( \sum_{j=1}^d \, (\xi_{t,k}-\xi_{t,j}) \tilde{\mu}_{t,j} \right) \, \tilde{\mu}_{t,k} \, dw_{t,1} \end{eqnarray} \]

(27)

\[ \begin{eqnarray} && + 2 \sqrt{\eta} \left( \sum_{j=1}^d \, (\pi_{t,k}-\pi_{t,j}) \tilde{\mu}_{t,j} \right) \, \tilde{\mu}_{t,k} \, dw_{t,2} \, . \\\end{eqnarray} \]

This dynamics corresponds to the QND measurement of the populations \( \tilde{\mu}_{t,k}\) of the qudit levels, with two measurement channels \( L_1(t) = \sum_{j=1}^d |j\rangle\langle j|\, \xi_{t,j}\) and \( L_2(t) = \sum_{j=1}^d |j\rangle\langle j|\, \pi_{t,j}\) .

The latter dynamics is relevant if it remains significant after the convergence of the \( \rho_{t,(k,k)}\) towards coherent states, thus leading to the statement in the main text.

6.3.2 Indistinguishable emission

We now move to the setting of Section 3.3.2. We will treat it in quite some detail in order to illustrate our method for finding deterministic manifold equations.

Algebraic criterion:

We first give the detailed computations concerning the algebraic criterion of Prop.1. After noting that \( [L_1,L_2] = 0\) and hence \( [G_{L_1},\; G_{L_2}]=0\) , we compute further commutation with the deterministic evolution. We compute \( [L_j^\dagger L_j , \; L_1 ] = \frac{1}{2}( \sigma_{-A}\pm\sigma_{zA}\sigma_{-B} + \sigma_{-B}\pm \sigma_{zB}\sigma_{-A})\) with signs depending on \( j \in \{1,2\}\) , and similarly for \( [L_2,\; L_j^\dagger L_j ] \) . Taken separately, this corresponds to two new vector fields \( G_{L'_k}\) with \( L'_1 = \sigma_{zA}\sigma_{-B} + \sigma_{zB}\sigma_{-A}\) and \( L'_2 = i (\sigma_{zA}\sigma_{-B} - \sigma_{zB}\sigma_{-A})\) , whose further commutations happen to generate yet other directions. When the individual channels \( L_1\) and \( L_2\) have arbitrary rates, \( \mathfrak{G}_F\) contains all these vector fields and the model reduction would not be efficient. However, when the rates of \( F_{L_1}\) and \( F_{L_2}\) are equal (and thus, without requiring \( \eta_1=\eta_2\) since they do not appear there), we see instead that the commutator with their sum yields no new diffusion directions; you can see this thanks to the opposite signs in the above individual commutators.

One can further check that when adding nonzero drives in \( \sigma_x\) and/or \( \sigma_y\) on A and/or B, under any conditions, the diffusion spans manifolds of dimension 10 — hence, expect no easy explicit formula for the solution. Adding detuning, i.e. a Hamiltonian in \( \sigma_{z,A}\) or \( \sigma_{z,B}\) , just doubles the manifold to dimension 4.

Stochastic differential equations:

As stated in the main text, towards writing the deterministic manifold equations, we translate the dynamics (15) to the Pauli basis.

  • In fact, as the ground state on any qubit should be invariant, we readily introduce displaced Z variables, replacing \( r(Zq),\; r(qZ),\; r(ZZ)\) respectively by \( r(Zq^*) = r(Zq)-r(Iq),\; r(qZ^*) = r(qZ)-r(qI),\; r(ZZ^*)=r(ZZ)-r(ZI)-r(IZ)\) for \( q\in \{I,X,Y\}\) . The corresponding equations follow systematically, e.g. 

    \[ \begin{eqnarray*} dr(XI)_t &=& -r(XI)_t\, dt + \big( -r(ZI^*)_t + r(XX)_t - (r(XI)+r(IX))_t r(XI)_t \big) \, \sqrt{\eta_1}\, dw_{t,1}\\ && + \big( -r(XY)_t - (r(YI)-r(IY))_t\, r(XI)_t \big) \, \sqrt{\eta_2}\, dw_{t,2} \; . \end{eqnarray*} \]

    The others are similar and we do not write them all down here. Note that the output signals in this basis write:

    \[ dy_{t,1}= \sqrt{\eta_1} (r(XI)+r(IX))_t \; dt + dw_{t,1}\;\; , ~ dy_{t,2}= \sqrt{\eta_2} (r(YI)-r(IY))_t \; dt + dw_{t,2} \; . \]
  • We next group the variables in sums and differences, e.g. \( X_s = r(XI)+r(IX)\) , \( XY_d = r(XY)-r(YX)\) , \( YZ_s = r(YZ)+r(ZY)\) and so on. The dynamics are obtained as sums and differences, with no Itō specificities. This decouples the system into a block of 9 variables, not influenced by, yet influencing (block-triangular form), the 6 remaining ones \( X_d,\, Y_s,\, Z_d,\, XY_s, \, XZ_d,\, YZ_s\) .
  • We finally write the ratio between each of these variables and \( r(ZZ)_t\) , computing the resulting dynamics with due Itō corrections. Using \( dy_{t,1}\) and \( dy_{t,2}\) to include the stochastic contributions, this yields the following rather compact dynamics:

    \[ \begin{eqnarray*} dB_{1,t} &=& B_{1,t}\, dt - 2 \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_1 = YZ_d / r(ZZ)\\ dB_{2,t} &=& B_{2,t}\, dt - 2 \sqrt{\eta_1}\, dy_{t,1} ~ \text{for } B_2 = XZ_s / r(ZZ)\\ dB_{3,t} &=& 2 B_{3,t}\, dt + B_{1,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_3 = r(YY) / r(ZZ)\\ dB_{4,t} &=& 2 B_{4,t}\, dt - B_{2,t} \sqrt{\eta_1}\, dy_{t,1} ~ \text{for } B_4 = r(XX) / r(ZZ)\\ dB_{5,t} &=& 2 B_{5,t}\, dt + B_{1,t} \sqrt{\eta_1}\, dy_{t,1} + B_{2,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_5 = XY_d / r(ZZ)\\ dB_{6,t} &=& 2 B_{6,t}\, dt + B_{2,t} \sqrt{\eta_1}\, dy_{t,1} + B_{1,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_6 = Z_s / r(ZZ)\\ dB_{7,t} &=& 3 B_{7,t}\, dt + (2B_4-B_6)_t \sqrt{\eta_1}\, dy_{t,1} - B_{5,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_7 = X_s / r(ZZ)\\ dB_{8,t} &=& 3 B_{8,t}\, dt - B_{5,t} \sqrt{\eta_1}\, dy_{t,1} - (2B_3+B_6)_t \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_8 = Y_d / r(ZZ)\\ dB_{0,t} &=& 4 B_{0,t}\, dt + B_{7,t} \sqrt{\eta_1}\, dy_{t,1} + B_{8,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } B_0 = 1/ r(ZZ) \end{eqnarray*} \]

    concerning the first block of 9 variables, and

    \[ \begin{eqnarray*} dR_{1,t} &=& R_{1,t}\, dt ~ \text{for } R_1 = XZ_d / r(ZZ)\\ dR_{2,t} &=& R_{2,t}\, dt ~ \text{for } R_2 = YZ_s / r(ZZ) \\ dR_{3,t} &=& 2 R_{3,t}\, dt - R_{1,t} \sqrt{\eta_1}\, dy_{t,1} - R_{2,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } R_3 = Z_d / r(ZZ)\\ dR_{4,t} &=& 2 R_{4,t}\, dt - R_{2,t} \sqrt{\eta_1}\, dy_{t,1} + R_{1,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } R_4 = XY_s / r(ZZ)\\ dR_{5,t} &=& 3 R_{5,t}\, dt - R_{3,t} \sqrt{\eta_1}\, dy_{t,1} - R_{4,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } R_5 = X_d / r(ZZ)\\ dR_{6,t} &=& 3 R_{6,t}\, dt + R_{4,t} \sqrt{\eta_1}\, dy_{t,1} - R_{3,t} \sqrt{\eta_2}\, dy_{t,2} ~ \text{for } R_6 = Y_s / r(ZZ) \end{eqnarray*} \]

    for the remaining block of 6 variables. This is our basis for identifying deterministically evolving variables (like \( R_1\) and \( R_2\) already are).

A set of deterministically evolving variables:

We must identify 13 deterministic combinations out of the above 15 equations.

  • Since \( B_1\) and \( B_2\) each move by a different the stochastic measurement result \( dy_2\) or \( dy_1\) , we would keep those as representing the 2 stochastic variables.
  • We next try to eliminate the stochastic term involving just \( B_1\) in the expression of \( dB_{3,t}\) . By Itō calculus, we note that \( d(\frac{B_1^2}{2}) = \big(2 \frac{B_1^2}{2} + 2 \eta_2\big) \, dt - 2 B_1 \sqrt{\eta_2}\, dy_2\) , such that we can deduce

    \[ d\tilde{B}_{3,t} = (2 \tilde{B}_{3,t} + \eta_2)\, dt ~ \text{for } \tilde{B}_3 = (\tfrac{B_1^2}{4}+B_3) \; . \]

    A similar treatment with \( d(\frac{B_2^2}{2})\) and \( d(\frac{B_1 B_2}{2})\) yields

    \[ \begin{eqnarray*} d\tilde{B}_{4,t} &=& (2 \tilde{B}_{4,t} + \eta_1)\, dt ~ \text{for } \tilde{B}_4 = (\tfrac{B_2^2}{4}-B_4) \; ,\\ d\tilde{B}_{5,t} &=& 2 \tilde{B}_{5,t}\, dt ~ \text{for } \tilde{B}_5 = (\tfrac{B_1 B_2}{2}+B_5) \; . \end{eqnarray*} \]
  • The stochastic terms in \( dB_{6,t}\) must be eliminated with a combination of \( d(B_1^2)\) and \( d(B_2^2)\) . For the stochastic terms in \( dB_{7,t}\) and \( dB_{8,t}\) , first we use products like e.g. \( d(B_4 B_2)\) to cancel \( B_{4,t} \sqrt{\eta_1}\, dy_{t,1}\) , then we add cubic terms in \( B_1,\, B_2\) to eliminate the remaining terms. For \( dB_0\) , after \( d(B_7 B_2 + B_8 B_1)\) , adding \( d(B_3^2+B_4^2+B_5^2+B_6^2)\) cancels all stochastic terms.
  • A similar procedure is applied to the \( R_k\) , combining them in products with \( B_1,B_2\) . Overall, this yields the following final result.

Proposition 13

The system (15) is confined to a two-dimensional manifold and its solution can be written as follows (see above for notation). The dependence on measurement results is characterized by:

\[ \begin{eqnarray*} B_{1}(t) &=& B_{1}(0) \, e^t - 2\sqrt{\eta_2}\, \int_0^t \, e^{t-s} \, dy_{s,2} \;\; , ~ \text{for } \;\; B_1 = \tfrac{YZ_d}{r(ZZ)} \; , \\ B_{2}(t) &=& B_{2}(0) \, e^t -2\sqrt{\eta_1}\, \int_0^t \, e^{t-s} \, dy_{s,1} \;\; , ~ \text{for } \;\;B_2 = \tfrac{XZ_s}{r(ZZ)} \; . \end{eqnarray*} \]

The other variables evolve independently of the measurement results, according to:

\[ \begin{eqnarray*} \tilde{B}_3(t) &=& \tilde{B}_{3}(0) \, e^{2t} + \tfrac{\eta_2}{2}(e^{2t}-1) \;\; , ~~ \text{for }\;\; \tilde{B}_3 = (\tfrac{B_1^2}{4}+\tfrac{r(YY)}{r(ZZ)}) \; , \\ \tilde{B}_4(t) &=& \tilde{B}_{4}(0) \, e^{2t} + \tfrac{\eta_1}{2}(e^{2t}-1) \;\; , ~~ \text{for }\;\; \tilde{B}_4 = (\tfrac{B_2^2}{4}-\tfrac{r(XX)}{r(ZZ)}) \; , \\ \tilde{B}_5(t) &=& \tilde{B}_{5}(0) \, e^{2t} \;\; , ~~ ~~ ~~ ~~ \text{for } \;\;\tilde{B}_5 = (\tfrac{B_1 B_2}{2}+\tfrac{XY_d}{r(ZZ)}) \; , \\ \tilde{B}_6(t) &=& \tilde{B}_{6}(0) \, e^{2t} + \tfrac{\eta_1+\eta_2}{2}(e^{2t}-1) \;\; , ~ \text{for }\;\; \tilde{B}_6 = (\tfrac{B_1^2+B_2^2}{4}+\tfrac{Z_s}{r(ZZ)}) \; , \\ \tilde{B}_7(t) &=& \tilde{B}_{7}(0) \, e^{3t} \;\; , ~~ \text{for } \;\;\tilde{B}_7 = (B_4 B_2 - \tfrac{B_6 B_2}{2} - \tfrac{B_5 B_1}{2} - \tfrac{B_1^2 B_2}{4} - \tfrac{B_2^3}{4} +\tfrac{X_s}{r(ZZ)}) \; , \\ \tilde{B}_8(t) &=& \tilde{B}_{8}(0) \, e^{3t} \;\; , ~~ \text{for }\;\; \tilde{B}_8 = (-B_3 B_1 - \tfrac{B_5 B_2}{2} - \tfrac{B_6 B_1}{2} - \tfrac{B_2^2 B_1}{4} - \tfrac{B_1^3}{4} +\tfrac{Y_d}{r(ZZ)}) \; , \\ \tilde{B}_0(t) &=& \tilde{B}_0(0) \, e^{4t} + \big({ (\eta_1+\eta_2)\tilde{B}_6(0)+2\eta_1\tilde{B}_4(0)+2\eta_2\tilde{B}_3(0)+\tfrac{(\eta_1+\eta_2)^2}{2}+\eta_1^2+\eta_2^2 }\big)\, \tfrac{e^{4t}-e^{2t}}{2}\\ && ~~~~ + \big({ \tfrac{(\eta_1+\eta_2)^2}{2}+\eta_1^2+\eta_2^2 }\big)\, \tfrac{e^{4t}-1}{4} \; ,\\ && ~~~~~~~ \text{for } \;\;\tilde{B}_0 = (\tfrac{B_7 B_2}{2} + \tfrac{B_8 B_1}{2} + \tfrac{B_3^2 +B_4^2+B_5^2+B_6^2}{2} +\tfrac{1}{r(ZZ)}) \; , \\ \end{eqnarray*} \]
\[ \begin{eqnarray*} R_1(t) &=& R_1(0) \, e^t \;\; , ~~ \text{for } \;\; R_1 = \tfrac{XZ_d}{r(ZZ)} \; , \\ R_2(t) &=& R_2(0) \, e^t \;\; , ~~ \text{for } \;\; R_2 = \tfrac{YZ_s}{r(ZZ)} \; , \\ \tilde{R}_3(t) &=& \tilde{R}_3(0) \, e^{2t} \;\; , ~~ \text{for }\;\; \tilde{R}_3 = (-\tfrac{R_1 B_2}{2} - \tfrac{R_2 B_1}{2} +\tfrac{Z_d}{r(ZZ)}) \; , \\ \tilde{R}_4(t) &=& \tilde{R}_4(0) \, e^{2t} \;\; , ~~ \text{for }\;\; \tilde{R}_4 = (\tfrac{R_1 B_1}{2} - \tfrac{R_2 B_2}{2} +\tfrac{XY_s}{r(ZZ)}) \; , \\ \tilde{R}_5(t) &=& \big( \tilde{R}_5(0)+\tfrac{\eta_2-\eta_1}{4}\,R_1(0) \big) \, e^{3t} - \tfrac{\eta_2-\eta_1}{4} R_1(0) \, e^t \; , \\ && ~ \text{for }\;\; \tilde{R}_5 = (-\tfrac{R_3 B_2}{2} - \tfrac{R_4 B_1}{2} + \tfrac{R_2 B_1 B_2}{4} + \tfrac{R_1 B_2^2}{8} - \tfrac{R_1 B_1^2}{8} +\tfrac{X_d}{r(ZZ)}) \; , \\ \tilde{R}_6(t) &=& \big( \tilde{R}_6(0)+\tfrac{\eta_1-\eta_2}{4}\,R_2(0) \big) \, e^{3t} - \tfrac{\eta_1-\eta_2}{4} R_2(0) \, e^t \; , \\ && ~ \text{for }\;\; \tilde{R}_6 = (-\tfrac{R_3 B_1}{2} + \tfrac{R_4 B_2}{2} + \tfrac{R_1 B_1 B_2}{4} + \tfrac{R_2 B_1^2}{8} - \tfrac{R_2 B_2^2}{8} +\tfrac{Y_s}{r(ZZ)}) \; . \end{eqnarray*} \]

This is but one way to describe the dynamics, as combinations of these variables yield other deterministic expressions — e.g. \( R_1/R_2\) is constant — which the reader may set up according to preferences.

6.3.3 A qudit monitored through \( n\) harmonic oscillators

Finally, we consider the setting of Section 3.3.3. This will be similar in spirit to Section 6.2.2. We provide all details to illustrate a last time how the procedure with Wigner functions works.

Algebraic criterion:

The measurement vector fields \( G_\bf{{ b}_l}\) all commute. Commutation with the deterministic terms, for \( u_t=v_t=0\) , yield linear combinations of the \( \bf{ a}_k\) , possibly premultiplied by \( |j\rangle\langle j|\) . Explicitly, writing \( \bf{ q} = \sum_j q_{j,k}\; |j\rangle\langle j| \otimes \bf{ a}_k\) , one commutation of \( G_\bf{{ q}}\) with the deterministic vector field amounts to the linear map:

\[ \begin{equation} q_{j,k} \mapsto \left(\, {\bf I}_d \otimes (\beta \beta^\dagger + i \Delta) + i X \, \right) \; q_{j,k} \; , \end{equation} \]

(28)

where \( q_{j,k}\) is considered a column vector, in tensor product structure of the \( j\) and \( k\) coordinates; column \( l\) of the matrix \( \beta\) contains the components \( \beta_{l,k}\) ; matrix \( \Delta\) is diagonal with components \( \Delta_k\) ; and matrix \( X\) is diagonal with components \( \chi_{j,k}\) (according to the same tensor product structure).

For generic values of \( \Delta, X, \beta\) , independently of the number of measurement channels \( m\) , the map (28) generates all \( 2 d n\) independent real linear combinations of \( \{\, |j\rangle\langle j| \otimes \bf{ a}_k , \; i|j\rangle\langle j| \otimes \bf{ a}_k : j=1,...,d ; k=1,...,n \, \}\) . By commuting the latter with the drive terms, in \( u_t\) and \( v_t\) , we obtain contributions in \( G_{|j\rangle\langle j| \otimes \bf{ I}}\) and \( G_{i|j\rangle\langle j| \otimes \bf{ I}}\) . Thus, taking into account that \( G_{i\mathbf{I}} = G_{\mathbf{I}}=0\) , in total the dimension of the manifold on which measurement outputs can spread the state is \( 2 d (n+1)-2\) , in presence of control signals and for general initial conditions; for \( u_t=v_t=0\) it reduces to dimension \( 2d n\) .

Stochastic differential equations:

Like for our other examples with harmonic oscillators, we consider their Wigner function representation, involving a Gaussian kernel to model the low stochastic dimension.

  • Thanks to the dispersive coupling with the qudit, we can write

    \[ \begin{equation} \rho_{t} = \sum_{j,j'=1}^d\; |j\rangle\langle j'| \otimes \rho_{t,(j,j')} \; , \end{equation} \]

    (29)

    where each \( \rho_{t,(j,j')}\) is an operator on the Hilbert space of the \( n\) cavities. For \( j=j'\) , these are unnormalized density operators, while for \( j \neq j'\) they need not be hermitian nor positive. Conditioned on the measurement results, the \( \rho_{t,(j,j')}\) evolve independently of each other. Indeed, the only place where one qudit level can influence another, is when taking the trace to define the \( dy_{t,l}\) .

  • We represent each \( \rho_{t,(j,j')}\) via its multi-variate Wigner function \( \mathcal{W}^{\{\rho_{t,(j,j')}\}}(q)\) . This is just the straightforward generalization of the single oscillator case, i.e. a pseudo-probability distribution over \( 2n\) variables, corresponding to the column vector \( q=(x_1,p_1,x_2,p_2,...,x_n,p_n)\) . Taking its marginal with respect to e.g. \( (p_1,x_2,p_3,x_4,...)\) gives the (truly real) probability distribution for a measurement of \( x_1 \otimes p_2 \otimes x_3 \otimes ...\) which is indeed a valid observable. By using the translations to Wigner space of annihilation and creation operators acting on \( \rho\) , as recalled right before Section 6.2.2, the stochastic master equation (16),(17) translates into:

    \[ \begin{eqnarray} \nonumber d\mathcal{W}^{(j,j')}_t &=& \sum_{k=1}^n \; \left(u_{t,k} \frac{\partial}{\partial p_k} - v_{t,k} \frac{\partial}{\partial x_k} \right) \, \mathcal{W}^{(j,j')}_t\, dt + \delta_k^{(j,j')}\; \left(x_k \frac{\partial}{\partial p_k} - p_k \frac{\partial}{\partial x_k} \right) \, \mathcal{W}^{(j,j')}_t\,dt \\ && + \sum_{k=1}^n \; - i\, \omega_k^{(j,j')} \; \left( 2\, x_k^2 + 2\, p_k^2 -1 -\frac{1}{8}\frac{\partial^2}{\partial x_k^2} - \frac{1}{8}\frac{\partial^2}{\partial p_k^2} \right) \, \mathcal{W}^{(j,j')}_t\,dt \end{eqnarray} \]

    (30)

    \[ \begin{eqnarray} && + \sum_{l,k,k'} \beta_{l,k} \bar{\beta}_{l,k'} \; \left( \mathbf{1}_{k,k'}+ \tfrac{1}{8}(\tfrac{\partial}{\partial x_k} + i \tfrac{\partial}{\partial p_k})(\tfrac{\partial}{\partial x_{k'}} - i \tfrac{\partial}{\partial p_{k'}})\right) \mathcal{W}^{(j,j')}_t\,dt \\ \nonumber && + \sum_{l,k,k'} \frac{\beta_{l,k} \bar{\beta}_{l,k'}}{4} \; \left(\, (x_k+i p_k )(\tfrac{\partial}{\partial x_{k'}} \text{-} i \tfrac{\partial}{\partial p_{k'}}) +(x_{k'}\text{-}i p_{k'}) (\tfrac{\partial}{\partial x_{k}} + i \tfrac{\partial}{\partial p_{k}}) \, \right) \mathcal{W}^{(j,j')}_t\,dt \\ \nonumber && + \sum_{l=1}^m \, 2 \sqrt{\eta_l} \left(\sum_{k=1}^n \mathfrak{R}(\beta_{l,k})\left(x_k + \tfrac{1}{4}\tfrac{\partial}{\partial x_k}\right) - \mathfrak{I}(\beta_{l,k})\left(p_k + \tfrac{1}{4}\tfrac{\partial}{\partial p_k}\right) - s_l \right)\, \mathcal{W}^{(j,j')}_t \; dw_{t,l} \; . \\\end{eqnarray} \]

    Here \( \delta_k^{(j,j')} = \Delta_k + \frac{\chi_{j,k}+\chi_{j',k}}{2}\) ; \( \omega_k^{(j,j')} = \frac{\chi_{j,k}-\chi_{j',k}}{2}\) ; the indicator function \( \mathbf{1}_{k,k'}\) equals 1 if \( k=k'\) and 0 otherwise; \( \bar{a}\) denotes the complex conjugate of \( a\) (without transpose, for vectors and matrices, i.e. \( \bar{a}^\dagger\) is the transpose of \( a\) ); \( \mathfrak{R}\) and \( \mathfrak{I}\) respectively denote real and imaginary part; and the measurement results are described by

    \[ \begin{equation} dy_{t,l} = 2 \sqrt{\eta_l}\, s_l\, dt + dw_{t,l} \; = \; 2 \sqrt{\eta_l}\, \sum_k (\; \mathfrak{R}(\beta_{l,k}) \text{Tr}(\rho_t \, \mathbf{X}_k) - \mathfrak{I}(\beta_{l,k}) \text{Tr}(\rho_t \, \mathbf{P}_k) \; ) \, dt + dw_{t,l} \; . \end{equation} \]

    (31)

    In a more compact notation, we have:

    \[ \begin{eqnarray} \nonumber d\mathcal{W}^{(j,j')}_t &=& \left(\, u^\dagger (\mathbf{I}_n \otimes J) + q^\dagger (\delta^{(j,j')} \otimes J) \,\right)\, \text{grad}_q \, \mathcal{W}^{(j,j')}_t\,dt \\ \nonumber && \; -i\,\left(\, q^\dagger (2\omega^{(j,j')} \otimes \mathbf{I}_2) q - \text{Tr}(\omega^{(j,j')}) - \tfrac{1}{8}\text{Tr}( (\omega^{(j,j')} \otimes \mathbf{I}_2)\, \text{hess}_{q} )\, \right) \, \mathcal{W}^{(j,j')}_t\,dt \\ \nonumber && + \left( \frac{1}{2}\text{Tr}(\tilde{R}) + \frac{1}{2} q^\dagger \tilde{R}\, \text{grad}_q + \frac{1}{8}\text{Tr}( \tilde{R}\, \text{hess}_q) \right) \, \mathcal{W}^{(j,j')}_t\,dt \\ && + \sum_{l=1}^m \, 2 \sqrt{\eta_l} \left( \beta_{l,A}^\dagger q + \tfrac{1}{4}\beta_{l,A}^\dagger\, \text{grad}_q - s_l \right) \mathcal{W}^{(j,j')}_t \; dw_{t,l} \; ; \end{eqnarray} \]

    (32)

    \[ \begin{eqnarray} dy_{t,l} &=& 2 \sqrt{\eta_l}\, \beta_{l,A}^\dagger \, Q_{t} \; dt + dw_{t,l} \; . \\\end{eqnarray} \]

    (33)

    Here \( J=[0 \; ,\; 1 \; ;\; -1 \; ,\; 0 ] \in \mathbb{R}^{2 \times 2}\) ; the diagonal matrices \( \delta^{(j,j')}\) and \( \omega^{(j,j')}\) \( \in \mathbb{R}^{n \times n}\) contain e.g. \( \delta_k^{(j,j')}\) as component \( k\) ; the vector \( u \in \mathbb{R}^2\) contains the control inputs in natural order; \( \text{grad}_q\) and \( \text{hess}_q\) respectively denote the gradient and the hessian with respect to \( q\) ; and column vectors \( \beta_{l,A} = [\mathfrak{R}(\beta_{l,1}),\; -\mathfrak{I}(\beta_{l,1}),\; \mathfrak{R}(\beta_{l,2}),\; -\mathfrak{I}(\beta_{l,2}),\; ... ]\) , \( Q_{t} = [\,\text{Tr}(\rho_t\, \mathbf{X}_1),\;\text{Tr}(\rho_t\, \mathbf{P}_1),\;\text{Tr}(\rho_t\, \mathbf{X}_2),\;\text{Tr}(\rho_t\, \mathbf{P}_2),\;... \,] \; \in \mathbb{R}^{2n}\) . We have further defined

    \[ \begin{eqnarray*} \tilde{R} &=& \sum_{l=1}^m \; R^{(re)}_l \otimes I_2 + R^{(im)}_l \otimes J ~ \in \mathbb{R}^{2n \times 2n}\\ && \text{with } R^{(re)}_{l,(k,k')} = \mathfrak{R}(\beta_{l,k}\bar{\beta}_{l,k'}) \;\; \text{ and } \;\; R^{(im)}_{l,(k,k')} = \mathfrak{I}(\beta_{l,k}\bar{\beta}_{l,k'}) \; . \end{eqnarray*} \]

    Note that \( \tilde{R}\) is real symmetric and \( \text{Tr}(\tilde{R}) = 2 \sum_l \beta_{l,A}^\dagger \beta_{l,A}\) . For the single cavity setting of Section 6.3.1, we just have \( \tilde{R}=2\, \mathbf{I}_{2n}\) . For further compactness, we will use below the notation \( \tilde{J} = (\mathbf{I}_n \otimes J)\) , \( \tilde\delta^{(j,j')} = (\delta^{(j,j')} \otimes J)\) and \( \tilde\omega^{(j,j')} = -i(\omega^{(j,j')} \otimes \mathbf{I}_2)\) . All these matrices belong to \( \mathbb{C}^{2n \times 2n}\) , the first two are real skew-symmetric and the last one is imaginary diagonal; they are thus all skew-hermitian, i.e. generators of rotations, as one would guess from the parameters they involve.

  • Describing a function of \( 2n\) variables involves, in full generality, a number of variables which is exponential in \( n\) . In the present case, thanks to the low-dimensional confinement, we can reduce this complexity essentially to the initial state only: from there, the evolution in time involves a Gaussian and thus a number of variables at most quadratic in \( n\) . Moreover, in agreement with the algebraic criterion, the number of variables influence by the stochastic measurement results is only linear in \( n\) . Explicitly, we write

    \[ \begin{eqnarray} \mathcal{W}^{\{\rho_{t,(j,j')}\}}(q) &=& \frac{\mu_t^{(j,j')}}{\pi^{n}\text{det}(S_t^{(j,j')})^{1/2}}\int \mathcal{W}^{\{\rho_0^{(j,j')}/\mu_0^{(j,j')}\}}(q_0) \, K^{(j,j')}_{t}(q,q_0)\, dq_0 \; , \end{eqnarray} \]

    (34)

    \[ \begin{eqnarray} K^{(j,j')}_{t}(q,q_0) &=& \exp\Bigg[-\left(q\text{-}\bar{\gamma}^{(j,j')}_t\text{-}\bar{M}^{(j,j')}_t q_0\right)^\dagger\; (S_t^{(j,j')})^{-1}\; \left(q\text{-}\gamma^{(j,j')}_t\text{-}M^{(j,j')}_t q_0\right) \\ \nonumber && \phantom{KKKKKKKKK} \; + q_0^\dagger D_t^{(j,j')} q_0 + (\bar{\lambda}^{(j,j')})^\dagger q_0 \; \Bigg] \; . \\\end{eqnarray} \]

    The time-dependent parameters whose equations we seek are scalars \( \mu_t^{(j,j')} \in \mathbb{C}\) ; vectors \( \gamma_t^{(j,j')}\) and \( \lambda_t^{(j,j')}\) \( \in \mathbb{C}^{2n}\) ; and matrices \( S_t^{(j,j')}\) , \( M_t^{(j,j')}\) and \( D_t^{(j,j')}\) \( \in \mathbb{C}^{2n \times 2n}\) . For \( j=j'\) , these parameters are all real. For \( j \neq j'\) , they can be complex and we have introduced some (not transposed) conjugates e.g. \( \bar{\gamma}_t^{(j,j')}\) to simplify expressions below. By analogy with Section 6.3.1, we have anticipated that the variables in latin letter will evolve deterministically, while those in greek letters will involve a stochastic component.

    In order to reach the correct dimension \( 2d(n+1)-2\) for the deterministically evolving manifold containing all trajectories, we can view the \( \gamma^{(j,j)}\) as independent stochastic variables (thus \( (2n)d\) real values), as well as part of the \( \mu^{(j,j')}\) (covering the \( 2d-2\) remaining variables); all the other variables, in particular the \( \lambda^{(j,j')}\) and the \( \gamma^{(j\neq j')}\) , will be deterministically related to them.

  • We next express \( d\mathcal{W}^{(j,j')}_t\) in two ways. On the left-hand side, viewing \( \mathcal{W}^{(j,j')}_t\) as a function of the Gaussian parameters, we express it with \( d\mu_{t,(j,j')}, d\gamma_t^{(j,j')}, ...\) , going up to second order Taylor expansion of the Gaussian in order to cover the Itō correction. On the right-hand side, viewing \( \mathcal{W}^{(j,j')}_t\) as a function of \( q\) , we compute the right-hand side of (32) for the particular Gaussian form (34). By separating, under the integral, the terms involving various powers of \( q, q_0\) and the deterministic and stochastic parts, we obtain the following set of equations. To reduce clutter, we drop the indices \( ^{(j,j')}\) and introduce \( Z_t=-S_t^{-1}\) :

    \[ \begin{align} q^\dagger\, & dZ_t\, q + \tfrac{1}{2} q^\dagger (Z_t+\bar{Z}_t^\dagger) d\gamma_t\, d\bar{\gamma}_t^\dagger (Z_t+\bar{Z}_t^\dagger)^\dagger \, q \end{align} \]

    (35)

    \[ \begin{align} \nonumber & \;\; = q^\dagger\, [\tilde{\delta},\, Z_t]\, q \, dt + \tfrac{1}{2} q^\dagger\, \{ \tilde{R},\, Z_t \} \, q \, dt + 2 q^\dagger \, \tilde{\omega} \, q \, dt + \tfrac{1}{8} q^\dagger\, (Z_t+\bar{Z}_t^\dagger)\, (\tilde{R} - \tilde{\omega})\, (Z_t+\bar{Z}_t^\dagger) \, q \, dt \\ \nonumber q_0^\dagger\, & dD_t \, q_0 + q_0^\dagger\, (d\bar{M}^\dagger_t Z_t M_t + \bar{M}^\dagger_t Z_t dM_t) \, q_0 + q_0^\dagger \, (\bar{M}^\dagger_t dZ_t M_t ) \, q_0 \\ + \tfrac{1}{2} & q_0^\dagger\, \left(d\lambda_t + \bar{M}_t^\dagger\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \right) \left(d\bar{\lambda}_t^\dagger + d\bar{\gamma}_t^\dagger (Z_t+\bar{Z}_t^\dagger) M_t \right) \, q_0 \end{align} \]

    (36)

    \[ \begin{align} \nonumber & \;\; = \tfrac{1}{8} \; q_0^\dagger\, \bar{M}^\dagger \, (Z_t+\bar{Z}_t^\dagger) \, (\tilde{R} - \tilde{\omega}) \, (Z_t+\bar{Z}_t^\dagger) \, M \, q_0 \, dt\\ \nonumber q_0^\dagger\, & \bar{M}_t^\dagger (dZ_t+d\bar{Z}_t^\dagger) \, q + q_0^\dagger\, d\bar{M}_t^\dagger (Z_t+\bar{Z}_t^\dagger) \, q + q_0^\dagger\, \left(d\lambda_t + \bar{M}_t^\dagger\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \right)d\bar{\gamma}_t^\dagger (Z_t+\bar{Z}_t^\dagger) \, q \\ & \;\; = -q_0^\dagger\, \bar{M}_t^\dagger (Z_t+\bar{Z}_t^\dagger)\, (\tilde{\delta}-\tfrac{1}{2}\tilde{R} \, q \, dt + \tfrac{1}{4} q_0^\dagger\, \bar{M}_t^\dagger (Z_t+\bar{Z}_t^\dagger)\,(\tilde{R}-\tilde{\omega})\,(Z_t+\bar{Z}_t^\dagger)\, q \, dt \end{align} \]

    (37)

    \[ \begin{align} \nonumber q^\dagger\, & (Z_t+\bar{Z}_t^\dagger)\, d\gamma_{t,\text{stochastic}} \\ & \;\; = -2 q^\dagger \, (\mathbf{I}_{2n}+\tfrac{Z_t+\bar{Z}_t^\dagger}{4})\; {\textstyle \sum_{l=1}^m} \; \sqrt{\eta_l} \, \beta_{l,A} \; dw_{t,l} \end{align} \]

    (38)

    \[ \begin{align} \nonumber q_0^\dagger\, & \left(\, d\lambda_{t,\text{stochastic}}+\bar{M}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_{t,\text{stochastic}}\, \right) \\ & \;\; = -2 q_0^\dagger \, \bar{M}^\dagger \, \tfrac{Z_t+\bar{Z}_t^\dagger}{4} \; {\textstyle \sum_{l=1}^m} \; \sqrt{\eta_l} \, \beta_{l,A} \; dw_{t,l} \end{align} \]

    (39)

    \[ \begin{align} \nonumber & \frac{d\mu_{t,\text{stochastic}}}{\mu_t}\, + \bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_{t,\text{stochastic}} \\ & \;\; = -2 {\textstyle \sum_{l=1}^m} \; \sqrt{\eta_l} \, \left( \bar{\gamma}_t^\dagger \, \tfrac{Z_t+\bar{Z}_t^\dagger}{4} \, \beta_{l,A} + s_l \right) \; dw_{t,l} \end{align} \]

    (40)

    \[ \begin{align} \nonumber q^\dagger\, & (dZ_t+d\bar{Z}_t^\dagger)\, \gamma_t + q^\dagger\,(Z_t+\bar{Z}_t^\dagger)\, d\gamma_{t,\text{det}} \\ \nonumber +& q^\dagger \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \frac{d\mu_t}{\mu_t} + q^\dagger\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t\, \bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \\ & \;\; = q^\dagger\,(Z_t+\bar{Z}_t^\dagger)\, \tilde{J} \, u_t \, dt + q^\dagger\, (\tilde{\delta}+ \tfrac{1}{2}\tilde{R})\, (Z_t+\bar{Z}_t^\dagger)\, \gamma_t \, dt \end{align} \]

    (41)

    \[ \begin{align} \nonumber & \;\; \phantom{=} \; + \tfrac{1}{4} q^\dagger\,(Z_t+\bar{Z}_t^\dagger)\, (\tilde{R}-\tilde{\omega}) \, (Z_t+\bar{Z}_t^\dagger)\, \gamma_t \, dt\\ \nonumber q_0^\dagger\, & d\lambda_{t,\text{det}} + q_0^\dagger\, \bar{M}^\dagger_t \, (dZ_t+d\bar{Z}_t^\dagger)\, \gamma_t + q_0^\dagger\, d\bar{M}_t^\dagger \, (Z_t+\bar{Z}_t^\dagger)\, \gamma_t + q_0^\dagger\, \bar{M}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_{t,\text{det}}\\ +& q_0^\dagger \left(\bar{M}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t + d\lambda_t \right)\; \left(\tfrac{d\mu_t}{\mu_t} + \bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \right) \end{align} \]

    (42)

    \[ \begin{align} \nonumber & \;\; = q_0^\dagger\, \bar{M}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, \tilde{J}\, u_t \, dt + \tfrac{1}{4}\, q_0^\dagger\,\bar{M}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\,(\tilde{R}-\tilde{\omega}) \, (Z_t+\bar{Z}_t^\dagger)\, \gamma_t\\ \nonumber & \frac{d\mu_{t,\text{det}}}{\mu_t} + \frac{d(\text{det}(Z_t)^{1/2})}{\text{det}(Z_t)^{1/2}} + \bar{\gamma}^\dagger_t\, dZ_t \, \gamma_t + \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_{t,det} \\ \nonumber + & d \bar{\gamma}^\dagger_t\, Z_t \, d\gamma_t + \tfrac{d\mu_t}{\mu_t} \, \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t + \tfrac{1}{2} \left( \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \right)^2 \\ & \;\; = \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, \tilde{J}\, u_t\, dt + \tfrac{1}{8} \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, (\tilde{R}-\tilde{\omega})\,(Z_t+\bar{Z}_t^\dagger)\, \gamma_t \, dt \end{align} \]

    (43)

    \[ \begin{align} & \;\; \phantom{=} \; + \tfrac{1}{2}\, \text{Tr}\left(\, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\,(\tilde{R}-\tilde{\omega}) \right)\, dt \; . \\\end{align} \]
  • Using (38)-(40), we express all the quadratic terms appearing on the left-hand side of the other equations, i.e. the Itō terms:

    \[ \begin{align} & (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \, d\bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger) = 4 (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, B \, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, dt \end{align} \]

    (44)

    \[ \begin{align} & \left(\, d\lambda_t +\bar{M}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t\, \right) \left( d\bar{\lambda}^\dagger_t + d\bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, M_t \right) = 4 \bar{M}^\dagger_t\, \tfrac{Z_t+\bar{Z}_t^\dagger}{4} \, B \, \tfrac{Z_t+\bar{Z}_t^\dagger}{4} \, M_t \, dt \end{align} \]

    (45)

    \[ \begin{align} & \left(\, d\lambda_t +\bar{M}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t\, \right) \, d\bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger) = \bar{M}^\dagger_t\,(Z_t+\bar{Z}_t^\dagger)\, B \, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4}) \; dt \end{align} \]

    (46)

    \[ \begin{align} & (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \, \left( \tfrac{d\mu_t}{\mu_t} + \bar{\gamma}^\dagger_t (Z_t+\bar{Z}_t^\dagger) d\gamma_t \right) = 4\, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, Z_t\, dt \end{align} \]

    (47)

    \[ \begin{align} \nonumber & \phantom{KKKK} \text{ with } Z_t = B \, \tfrac{Z_t+\bar{Z}_t^\dagger}{4}\, \gamma_t + {\textstyle \sum_l }\; \eta_l s_l \, \beta_{l,A} \\ & \left(\bar{M}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t + d\lambda_t \right)\; \left(\tfrac{d\mu_t}{\mu_t} + \bar{\gamma}^\dagger_t \, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \right) = 4 \bar{M}^\dagger_t \, \tfrac{Z_t+\bar{Z}_t^\dagger}{4} \, Z_t \, dt \end{align} \]

    (48)

    \[ \begin{align} & d\bar{\gamma}^\dagger_t \, Z_t \, d\gamma_t = 2\, \text{Tr}\left(\, (Z_t+\bar{Z}_t^\dagger)^{-1} \, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, B\, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, \right) \, dt \end{align} \]

    (49)

    \[ \begin{align} & \tfrac{d\mu_t}{\mu_t} \, \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t + \tfrac{1}{2} \left( \bar{\gamma}^\dagger_t\, (Z_t+\bar{Z}_t^\dagger)\, d\gamma_t \right)^2 \end{align} \]

    (50)

    \[ \begin{align} & \phantom{KKK} = 4 \bar{\gamma}^\dagger_t\, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, Z_t \, dt - 2 \bar{\gamma}^\dagger_t (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, B \, (\mathbf{I}_{2n} + \tfrac{Z_t+\bar{Z}_t^\dagger}{4})\, \gamma_t \, dt \\\end{align} \]

    Here we have introduced \( B = \sum_{l=1}^m \eta_l \beta_{l,A}\beta_{l,A}^\dagger \; \in \mathbb{R}^{2n \times 2n}\) . For the single cavity setting of Section 6.3.1, we just have \( B = \eta\, \mathbf{I}_{2n}\) .

A set of deterministically evolving variables:

We solve these equations sequentially.

  • First, from (35) and (44), we obtain an autonomous, deterministic equation for \( Z_t\) , and thus for \( S_t\) in the original formulation. Decomposing it in a symmetric part \( Z_S=(Z+\bar{Z}^\dagger)/2\) and a skew-symmetric one \( Z_A=(Z-\bar{Z}^\dagger)/2\) , we get:

    \[ \begin{eqnarray} \tfrac{d}{dt} Z_S &=& [\tilde{\delta},\, Z_S] + \tfrac{1}{2} \{ \tilde{R},\, Z_S\} + 2 \tilde\omega + \tfrac{1}{2} Z_S (\tilde{R}-\tilde{\omega}) Z_S - 2 (\mathbf{I}_{2n}+\tfrac{Z_S}{2}) B (\mathbf{I}_{2n}+\tfrac{Z_S}{2}) \; , \end{eqnarray} \]

    (51)

    \[ \begin{eqnarray} \tfrac{d}{dt} Z_A &=& [\tilde{\delta},\, Z_A] + \tfrac{1}{2} \{ \tilde{R},\, Z_A\} \; . \end{eqnarray} \]

    (52)

    Starting with \( Z_{A,0}=0\) at \( t=0\) , we will have \( Z_{A,t}=0\) for all times. We can thus identify \( Z_t = Z_{S,t}\) . We are not going to explicitly integrate (51) here, but one can note that it asymptotically converges (modulo generic appropriate observation conditions) towards the stationary point \( Z_t = -2 \, \mathbf{I}_{2n}\) . We report below its translation back to \( S_t\) .

  • Next, replacing the previous point in (37) and using (46), we obtain a deterministic equation for \( M_t\) , depending on \( S_t\) :

    \[ \tfrac{d}{dt} M_t = \tilde{\delta}\, M_t - 2 Z_t^{-1} \tilde{\omega}\, M_t - \tfrac{1}{2} \tilde{R} \, M_t + 2 Z_t^{-1} (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, B \, M_t \; . \]

    This is a linear equation, but nontrivial, since \( M_{0} \neq 0\) and \( Z_t\) is time-varying. Once \( Z_t\) has converged to \( Z_t = -2 \, \mathbf{I}_{2n}\) (if we can say so, since there is no reason for such timescale separation), it would become a time-independent linear equation, involving rotation of \( M_t\) with \( \tilde{\delta},\tilde{\omega}\) and exponential decay with rate \( \tilde{R}/2\) .

  • Next, we can replace the preceding results in (36), and using (45), we obtain \( D_t\) as an explicit integral on \( M_t\) :

    \[ \tfrac{d}{dt} D_t = 2 \bar{M}^\dagger_t\, \tilde{\omega}\, M_t - 2 \bar{M}^\dagger_t\, B \, M_t \; . \]

    This closes a first set of deterministic variables.

  • After inserting the corresponding Itō terms into (38),(41), we get the stochastic equation:

    \[ \begin{eqnarray} d\gamma_t &=& \tilde{J}\, u_t \, dt + \tilde{\delta} \, \gamma_t \, dt - \tfrac{1}{2} \tilde{R} \, \gamma_t \, dt - 2 Z_t^{-1} \tilde{\omega}\, \gamma_t\, dt \end{eqnarray} \]

    (53)

    \[ \begin{eqnarray} && + Z_t^{-1}\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, \left( 2\, B \gamma_t\, dt - {\textstyle \sum_l }\; \sqrt{\eta_l} \, \beta_{l,A} \, dy_{t,l} \right) \; , \\\end{eqnarray} \]

    where thus \( dy_{t,l}\) follows (31). These variables are too numerous to be all independent, according to the manifold dimension expected from the algebraic criterion. In fact, each \( \gamma_t^{(j \neq j')}\) can be expressed as a deterministic function of \( \gamma_t^{(j,j)}\) and \( \gamma_t^{(j',j')}\) \( \in \mathbb{R}^{2n}\) , such that those variables together contribute \( 2dn\) dimensions to the confining manifold. The deterministic link goes as follows.

    First, define \( L_t^{(j,j')} = Z_t^{(j,j')}\, \left(\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j')}}{2}\right)^{-1} \, \gamma_t^{(j,j')}\) . This results in

    \[ \begin{equation} dL_t^{(j,j')} = Z_t^{(j,j')}\, \left(\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j')}}{2} \right)^{-1} \tilde{J}\, u_t \, dt -{\textstyle \sum_l}\; \sqrt{\eta_l} \beta_{l,A}\, dy_{t,l} \; + \left( \tilde{\delta}^{(j,j')} - \tilde{\omega}^{(j,j')} + \tfrac{\tilde{R}}{2} \right) \, L_t^{(j,j')} \; . \end{equation} \]

    (54)

    Any linear combination \( \sum_{j,j'} \; C^{(j,j')}\; L_t^{(j,j')}\) with coefficients satisfying \( \sum_{j,j'} \; C^{(j,j')} = 0\) would cancel the explicit dependence on measurements \( dy_{t,l}\) .

    The remaining issue is to find a linear combination which also provides an autonomous deterministic term, thus avoiding indirect dependence on the measurements.

    • The term in \( dy_{t,l}\) will cancel as soon as \( \sum_{j,j'} \; C^{(j,j')} = 0\) . Note that the property also holds if the \( C^{(j,j')} \in \mathbb{C}^{2n \times 2n}\) are time-dependent.
    • The term in \( \tilde{J}\, u_t \, dt\) will be an autonomous deterministic contribution, as long as the \( C^{(j,j')}_t\) only depend on deterministic variables.
    • The term in \( \tilde{R}\) is independent of \( (j,j')\) . Hence, if we take \( X^{(j,j')}\) a scalar linear combination of the \( L^{(j,j')}\) , then it would lead to a term proportional to \( \tilde{R}\; X^{(j,j')}\) , which is compatible with an autonomous equation for \( X^{(j,j')}\) . If the \( C^{(j,j')}\) are matrix coefficients, then the result of their commutation with \( \tilde{R}\) will have to be investigated.
    • Unfortunately, the term in \( \tilde{\delta}^{(j,j')}-\tilde{\omega}^{(j,j')}\) is not of this type, calling for a more complicated solution. However, we observe that (i) these are all rotations and (ii) if we take the triplet \( (j\neq j'),\; (j,j),\; (j',j')\) , then their corresponding coefficients are linearly related.

This last observation is the key towards proposing two things. First, we will search for deterministic variables as a linear combination of said triplet, thus

\[ \begin{equation} X^{(j,j')}_t \; = \; C^{(j,j',1)}_t \, L^{(j,j)}_t + C^{(j,j',2)}_t \, L^{(j',j')}_t + C^{(j,j',3)}_t \, L^{(j,j')}_t \; . \end{equation} \]

(55)

Second, we will decompose \( \tilde{\delta}^{(j,j')}-\tilde{\omega}^{(j,j')}\) into a mean contribution and a deviation:

\[ \begin{eqnarray} (\tilde{\delta}-\tilde{\omega})^{(j,j)} &=& \tilde{\delta}^{(j,j')} + \omega^{(j,j')} \otimes J \end{eqnarray} \]

(56)

\[ \begin{eqnarray} (\tilde{\delta}-\tilde{\omega})^{(j',j')} &=& \tilde{\delta}^{(j,j')} - \omega^{(j,j')} \otimes J \\ \nonumber (\tilde{\delta}-\tilde{\omega})^{(j,j')} &=& \tilde{\delta}^{(j,j')} + i\omega^{(j,j')} \otimes \mathbf{I}_2 \; . \\\end{eqnarray} \]

The first term on the right hand side is the same for all three cases, it thus plays a role similar to \( \tilde{R}\) . The second term depends on the row of (56), but it generates a rotation; moreover, all these terms commute since \( \delta^{(j,j')}\) and \( \omega^{(j,j')}\) are diagonal, and we recall \( \tilde{\delta}^{(j,j')} = \delta^{(j,j')} \otimes J\) . This suggests to cancel the row-dependent parts of (56) by going to a corresponding rotating frame, which would be transparent for the first, common term. The algebraic criterion, fixing the manifold dimension, encourages us the other terms should behave favorably.

We thus write:

\[ \begin{eqnarray} C^{(j,j',1)}_t &=& C^{(j,j',1)}_0 \, \exp\left(-(\omega^{(j,j')} \otimes J)\, t \right) \;\; , \end{eqnarray} \]

(57)

\[ \begin{eqnarray} C^{(j,j',2)}_t &=& C^{(j,j',2)}_0 \, \exp\left(+(\omega^{(j,j')} \otimes J)\, t \right) \;\; , \\ \nonumber C^{(j,j',3)}_t &=& C^{(j,j',3)}_0 \, \exp\left(-i(\omega^{(j,j')} \otimes \mathbf{I}_2)\, t \right) \; . \\\end{eqnarray} \]

The constraint \( \sum_{j,j'} \; C_t^{(j,j')} = 0\) for all \( t\) then imposes, up to pre-multiplying by the same constant matrix:

\[ \begin{equation} C^{(j,j',1)}_0 = \mathbf{I}_n \otimes \left(\begin{array}{cc} \tfrac{-1}{2} & \tfrac{i}{2} \\ \tfrac{-i}{2} & \tfrac{-1}{2} \end{array}\right) \; , ~ C^{(j,j',2)}_0 = \mathbf{I}_n \otimes \left(\begin{array}{cc} \tfrac{-1}{2} & \tfrac{-i}{2} \\ \tfrac{i}{2} & \tfrac{-1}{2} \end{array}\right) \; , ~ C^{(j,j',3)}_0= \mathbf{I}_{2n} \; . \end{equation} \]

(58)

One checks that these \( C^{(j,j',k)}_0\) , although not full-rank, commute with \( A \otimes J\) for any \( A\) , and of course with \( A \otimes \mathbf{I}_2\) . They thus maintain the property

\[ C^{(j,j',1)}_t \, \tilde{\delta}^{(j,j')} \, L^{(j,j)}_t + C^{(j,j',2)}_t \, \tilde{\delta}^{(j,j')} \, L^{(j',j')}_t + C^{(j,j',3)}_t \, \tilde{\delta}^{(j,j')} \, L^{(j,j')}_t = \tilde{\delta}^{(j,j')} \, X^{(j,j')}_t \; . \]

Finally, similar commutation properties, as well as the property

\[ \begin{eqnarray} \exp\left(-(\omega^{(j,j')} \otimes J)\, t \right)\, C^{(j,j',1)}_0 &=& e^{-i (\omega^{(j,j')}\otimes \mathbf{I}_2) t} \, C^{(j,j',1)}_0 \; , \end{eqnarray} \]

(59)

\[ \begin{eqnarray} \exp\left((\omega^{(j,j')} \otimes J)\, t \right)\, C^{(j,j',2)}_0 &=& e^{-i (\omega^{(j,j')} \otimes \mathbf{I}_2) t} \, C^{(j,j',2)}_0 \; , \\\end{eqnarray} \]

lead to the result:

\[ C^{(j,j',1)}_t \, \tilde{R} \, L^{(j,j)}_t + C^{(j,j',2)}_t \, \tilde{R} \, L^{(j',j')}_t + C^{(j,j',3)}_t \,\tilde{R} \, L^{(j,j')}_t = e^{\tilde{\omega}^{(j,j')} t} \, \tilde{R}\, e^{-\tilde{\omega}^{(j,j')} t} \, X^{(j,j')}_t \; . \]

In hindsight, (59) shows that \( \tilde{X}_t = e^{-\tilde{\omega}^{(j,j')} t} \, X_t = \; C^{(j,j',1)}_0\, L^{(j,j)}_t + C^{(j,j',2)}_0 \, L^{(j',j')}_t + C^{(j,j',3)}_0 \, L^{(j,j')}_t \; \) in fact undergoes deterministic dynamics. Taking all things together, we have

\[ \begin{eqnarray*} \tfrac{d}{dt}\tilde{X}^{(j,j')}_t & = & C^{(j,j',1)}_0 \, Z_t^{(j,j)}\, \left(\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j)}}{2} \right)^{-1} \tilde{J}\, u_t \;+\; C^{(j,j',2)}_0 \, Z_t^{(j',j')}\, \left(\mathbf{I}_{2n}+\tfrac{Z_t^{(j',j')}}{2} \right)^{-1} \tilde{J}\, u_t \\ && + Z_t^{(j,j')}\, \left(\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j')}}{2} \right)^{-1} \tilde{J}\, u_t \; +\;\; (\tilde{\delta}-\tilde{\omega}+ \tfrac{\tilde{R}}{2})^{(j,j')} \, \tilde{X}^{(j,j')}_t \end{eqnarray*} \]

as a deterministic variable, which together with the knowledge of \( \gamma^{(j,j)}_t\) and \( \gamma^{(j',j')}_t\) define:

\[ \begin{eqnarray} \gamma_t^{(j,j')} &=& \frac{\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j')}}{2}}{Z_t^{(j,j')}} \, \Bigg( \tilde{X}^{(j,j')}_t - C^{(j,j',1)}_0\, \frac{Z_t^{(j,j)}}{\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j)}}{2}}\; \gamma_t^{(j,j)} \end{eqnarray} \]

(60)

\[ \begin{eqnarray} && \phantom{ \frac{\mathbf{I}_{2n}+\tfrac{Z_t^{(j,j')}}{2}}{Z_t^{(j,j')}} \, \, \Bigg( X^{(j,j')}_t -} - C^{(j,j',2)}_0\, \frac{Z_t^{(j',j')}}{\mathbf{I}_{2n}+\tfrac{Z_t^{(j',j')}}{2}}\; \gamma_t^{(j',j')} \Bigg) \; . \\\end{eqnarray} \]
  • Next, now again separately for each \( (j,j')\) , consider (39),(42), in which \( d\gamma_t\) can be inserted from the last point. This readily yields

    \[ \begin{equation} d\lambda_t = 4 \bar{M}_t^\dagger\, \tilde{\omega} \, \gamma_t\, dt - 2 \bar{M}_t^\dagger\, \left( 2\, B \gamma_t\, dt - {\textstyle \sum_l }\; \sqrt{\eta_l} \, \beta_{l,A} \, dy_{l,t} \right) \; . \end{equation} \]

    (61)

    We recognize that the measurement-dependent term can be eliminated in a linear combination with \( d\gamma\) : defining

    \[ h_t = \gamma_t + Z_t^{-1}\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, \tfrac{(\bar{M}_t^\dagger)^{-1}}{2} \, \lambda_t \; , \]

    we obtain the autonomous deterministic evolution:

    \[ \tfrac{d}{dt} h_t = \tilde{J} \, u_t + \tilde{\delta}\, h_t - \tfrac{1}{2} \tilde{R} \, h_t + \tilde{\omega} \, h_t \; . \]

    For \( u_t=0\) , this would involve a matrix exponential inducing constant rotation and decay, in fact the same as for \( M_t\) when \( Z_t = -2 \, \mathbf{I}_{2n}\) . In any case, it establishes that \( \lambda_t^{(j,j')}\) is a purely deterministic function of \( \gamma_t^{(j,j')}\) , i.e. once \( \gamma_t^{(j,j')}\) is given, the value of \( \lambda_t^{(j,j')}\) is independent of the measurement results.

  • Last but not least, there remains to treat \( \mu_t\) . Inserting the Itō terms and the previous results into (40),(43) yields

    \[ \begin{eqnarray*} \frac{d\mu_{t}}{\mu_t} + \frac{d(\text{det}(Z_t)^{1/2})}{\text{det}(Z_t)^{1/2}} &=& 2 \sum_l \, \sqrt{\eta_l}\, (\beta_{l,A}^\dagger \gamma_t - s_l) \, dw_{t,l} \\ && + \tfrac{1}{4} \text{Tr}((\tilde{R}-\tilde{\omega})Z_t)\, dt + 2 \bar{\gamma}_t^\dagger \tilde{\omega}\, \gamma_t\, dt + \tfrac{1}{2} \text{Tr}(\tilde{R}-\tilde{\omega}) \, dt \\ && - \text{Tr}\left(\, B \, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, Z_t^{-1}\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, \right) \, dt \; . \end{eqnarray*} \]

    Inserting \( \frac{d(\text{det}(Z_t)^{1/2})}{\text{det}(Z_t)^{1/2}} = \tfrac{1}{2}\, \text{Tr}(Z_t^{-1}\, dZ_t)\) with \( dZ_t\) derived above, reduces this equation to:

    \[ \frac{d\mu_{t}}{\mu_t} = 2 \sum_l \, \sqrt{\eta_l}\, (\beta_{l,A}^\dagger \gamma_t - s_l) \, dw_{t,l} - \text{Tr}(\tilde{\omega}\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, Z_t^{-1})\, dt + 2 \bar{\gamma}_t^\dagger \, \tilde{\omega} \, \gamma_t\, dt \; . \]

    Taking into account that \( \mu^{(j,j')} = \bar{\mu}^{(j',j)}\) , these are \( d^2\) stochastic equations, whereas there should remain \( 2d-2\) independent stochastic variables. One way of parameterizing this is to consider the \( \mu^{(j=j')}\) as independent stochastic, thus following (recall that \( \tilde{\omega}^{(j,j')}=0\) for \( j=j'\) ):

    \[ \frac{d\mu^{(j,j)}_{t}}{\mu^{(j,j)}_t} \;=\; 2 \sum_l \, \sqrt{\eta_l}\, (\beta_{l,A}^\dagger \gamma^{(j,j)}_t - s_l) \, dw_{t,l} \; = \; 2 \sum_l \, \sqrt{\eta_l}\, \beta_{l,A}^\dagger (\gamma^{(j,j)}_t - Q_{t}) \, dw_{t,l}\; . \]

    These contribute \( d-1\) independent variables, as they are subject to one constraint fixing the total normalization. Like for the single-oscillator case, we see that \( \mu_t^{(j,j)}\) varies more if its Gaussian position \( \gamma^{(j,j)}\) deviates more from the total state mean positions \( Q_t\) .

    Next, we observe that the stochastic term comports one part that is independent of \( (j,j')\) — and could thus cancel when taking linear combinations of \( \mu^{(j,j')}\) — while the other part involves \( \gamma^{(j,j)}_t\) . To make such a term appear from another stochastic variable, we consider \( \Gamma_t = \bar{\gamma}_t^\dagger \, Z_t\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})^{-1}\, \gamma_t\) . A few computations then indeed yield:

    \[ \begin{eqnarray} d(\log(\mu)+\Gamma) &=& - 2 \sum_l\, \sqrt{\eta_l}\, s_l\, dw_{t,l} - 2 \sum_l \, \eta_l \, s_l^2 \, dt \end{eqnarray} \]

    (62)

    \[ \begin{eqnarray} && + \text{Tr}\left( B\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, Z_t^{-1}\, \right) \, dt - \text{Tr}(\tilde{\omega}\, (\mathbf{I}_{2n}+\tfrac{Z_t}{2})\, Z_t^{-1})\, dt \\ \nonumber && + 2\, L_t^\dagger \, \tilde{J} \, u_t \, dt \; , \\\end{eqnarray} \]

    with \( L_t\) essentially related to \( \gamma_t\) and following the stochastic equation (54). The first row of (62) is now totally independent of \( (j,j')\) . The second row only contains deterministic variables. In the last row, the presence of \( L_t\) still has to be handled. The idea, in order to obtain purely deterministic variables, is to take linear combinations of (62) for various \( (j,j')\) : its first row would disappear, while the last row would involve the deterministic variables \( \tilde{X}^{(j,j')}\) .

    For \( u_t=0\) , this is simple: the last row is absent, so any linear combination of \( (\log(\mu)+\Gamma)^{(j,j')}\) for various indices \( (j,j')\) would yield a purely deterministic equation, involving only the second row of (62), as soon as the coefficients of the linear combination sum to zero. This also shows that the \( \mu_t^{j,j}\) are not stochastically independent either in this case, as we have already seen for the single oscillator model. For \( u_t \neq 0\) , we have to make this slightly more complicated.

    First, consider the real part of (62). We would define

    \[ \begin{equation} Y^{(j,j')}_{R,t} = \tilde{c}^{(j,j',1)} \mathfrak{R}(\log(\mu)+\Gamma)^{(j,j)}+\tilde{c}^{(j,j',2)} \mathfrak{R}(\log(\mu)+\Gamma)^{(j',j')}+\tilde{c}^{(j,j',3)} \mathfrak{R}(\log(\mu)+\Gamma)^{(j,j')} \end{equation} \]

    (63)

    with scalars \( \tilde{c}^{(j,j',k)} \) satisfying \( \sum_k \, \tilde{c}^{(j,j',k)} = 0\) , in order for the first row of (62) to cancel when writing \( dY^{(j,j')}_{R,t}\) . We further note that all variables associated to \( j'=j\) are real, so from (58) we can write for the last row of (62):

    \[ \begin{eqnarray*} \tfrac{-1}{2}\, \mathfrak{R}\left( 2\, (L_t^{(j,j)})^\dagger \, \tilde{J} \, u_t \right) &=& \mathfrak{R}\left( 2\, (C_0^{(j,j',1)}\, L_t^{(j,j)})^\dagger \, \tilde{J} \, u_t \right)\; ,\\ \tfrac{-1}{2}\, \mathfrak{R}\left( 2\, (L_t^{(j',j')})^\dagger \, \tilde{J} \, u_t \right) &=& \mathfrak{R}\left( 2\, (C_0^{(j,j',2)}\, L_t^{(j',j')})^\dagger \, \tilde{J} \, u_t \right) \; , \end{eqnarray*} \]

    while \( C_0^{(j,j',3)}= \mathbf{I}_{2n}\) trivially implies:

    \[ \mathfrak{R}\left( 2\, (L_t^{(j,j')})^\dagger \, \tilde{J} \, u_t \right) = \mathfrak{R}\left( 2\, (C_0^{(j,j',3)}\, L_t^{(j,j')})^\dagger \, \tilde{J} \, u_t \right) \; . \]

    Therefore, taking \( \tilde{c}^{(j,j',1)}= \tilde{c}^{(j,j',2)}=-1/2\) and \( \tilde{c}^{(j,j',3)}=1\) in (63) is compatible with a fully deterministic evolution:

    \[ \begin{eqnarray*} \tfrac{d}{dt} Y^{(j,j')}_{R,t} &=& \frac{-1}{2}\, \text{Tr}\left( B\, (\mathbf{I}_{2n}+\tfrac{Z^{(j,j)}_t}{2})\, (Z_t^{(j,j)})^{-1}\, \right) - \frac{1}{2}\, \text{Tr}\left( B\, (\mathbf{I}_{2n}+\tfrac{Z^{(j',j')}_t}{2})\, (Z_t^{(j',j')})^{-1}\, \right) \\ && + \mathfrak{R}\left(\, \text{Tr}\left( \,(B-\tilde{\omega}^{(j,j')})\, (\mathbf{I}_{2n}+\tfrac{Z^{(j,j')}_t}{2})\, (Z_t^{(j,j')})^{-1}\, \right) \,\right)\\ && + 2\, \mathfrak{R}(\tilde{X}_t^{(j,j')})^\dagger \, \tilde{J} \, u_t \, . \end{eqnarray*} \]

    Since \( \mathfrak{R}\log(\mu) = \log(|\mu|)\) , this shows how the weights \( |\mu_t^{(j\neq j')}|\) are deterministically linked to the \( \mu_t^{(j,j)}\) and \( \gamma_t^{(j,j)}\) .

    There remains to find deterministic variables among the \( \mathfrak{I}\log(\mu^{(j,j')}) = \text{phase}(\mu^{(j,j')})\) . Taking the imaginary part of (62), the first row drops rightaway. Furthermore, from (58), we note that for any triplet \( j,j',j''\) one has:

    \[ \mathfrak{I}(L^{(j,j')}_t + L^{(j',j'')}_t + L^{(j'',j)}_t ) = \mathfrak{I}(\tilde{X}^{(j,j')}_t + \tilde{X}^{(j',j'')}_t + \tilde{X}^{(j'',j)}_t )\; . \]

    Therefore, we can define

    \[ \begin{equation} Y^{(j,j',j'')}_{I,t} = \mathfrak{I}(\log(\mu)+\Gamma)^{(j,j')}+ \mathfrak{I}(\log(\mu)+\Gamma)^{(j',j'')}+ \mathfrak{I}(\log(\mu)+\Gamma)^{(j'',j)} \end{equation} \]

    (64)

    and obtain its deterministic evolution:

    \[ \begin{eqnarray*} \tfrac{d}{dt}\, Y^{(j,j',j'')}_{I,t} &=& \mathfrak{I}\left(\, \text{Tr}\left( \,(B-\tilde{\omega}^{(j,j')})\, (\mathbf{I}_{2n}+\tfrac{Z^{(j,j')}_t}{2})\, (Z_t^{(j,j')})^{-1}\, \right) \,\right)\\ && + \mathfrak{I}\left(\, \text{Tr}\left( \,(B-\tilde{\omega}^{(j',j'')})\, (\mathbf{I}_{2n}+\tfrac{Z^{(j',j'')}_t}{2})\, (Z_t^{(j',j'')})^{-1}\, \right) \,\right)\\ && + \mathfrak{I}\left(\, \text{Tr}\left( \,(B-\tilde{\omega}^{(j'',j)})\, (\mathbf{I}_{2n}+\tfrac{Z^{(j'',j)}_t}{2})\, (Z_t^{(j'',j)})^{-1}\, \right) \,\right)\\ && + 2 \, \mathfrak{I}(\tilde{X}^{(j,j')}_t + \tilde{X}^{(j',j'')}_t + \tilde{X}^{(j'',j)}_t )^\dagger \, \tilde{J} \, u_t \, . \end{eqnarray*} \]

    This expresses how the phases of the \( \mu^{(j,j')}_t\) are deterministically linked. One can check that for instance the phases of \( \mu^{(1,2)}_t,\,\mu^{(1,3)}_t,...,\mu^{(1,d)}_t\) can be chosen independently, then constraining all the other phases through the \( Y^{(j,j',j'')}_{I,t}\) , in agreement with the fact that there remained to find \( (d-1)\) stochastic variables and all other deterministic.

This concludes the computations. There remains to define the initial conditions, by imposing the Gaussian kernel to coincide with the Dirac-peak limit at \( t=0\) . We have thus established the following result.

Proposition 14

The quantum SDE (16),(17), for a general initial condition, admits the explicit solution:

\[ \rho_{t} = \sum_{j,j'=1}^d\; |j\rangle\langle j'| \otimes \rho_{t,(j,j')} \; , \]

where each \( \rho_{t,(j,j')}\) is an operator on the Hilbert space of the \( n\) cavities. The evolution of the latter is described as follows in its Wigner function representation:

\[ \begin{eqnarray} \mathcal{W}^{\{\rho_{t,(j,j')}\}}(q) &=& \frac{\mu_t^{(j,j')}}{\pi^{n}\mathrm{det}(S_t^{(j,j')})^{1/2}}\int \mathcal{W}^{\{\rho_0^{(j,j')}/\mu_0^{(j,j')}\}}(q_0) \, K^{(j,j')}_{t}(q,q_0)\, dq_0 \; , \end{eqnarray} \]

(65)

\[ \begin{eqnarray} K^{(j,j')}_{t}(q,q_0) &=& \exp\Bigg[-\left(q-\bar{\gamma}^{(j,j')}_t-\bar{M}^{(j,j')}_t q_0\right)^\dagger\; (S_t^{(j,j')})^{-1}\; \left(q-\gamma^{(j,j')}_t-M^{(j,j')}_t q_0\right) \\ \nonumber && \phantom{KKKKKKKKK} \; + q_0^\dagger D_t^{(j,j')} q_0 + (\bar{\lambda}^{(j,j')})^\dagger q_0 \; \Bigg] \; . \\\end{eqnarray} \]

Defining the constants:

\[ \begin{align*} & \tilde{R} = \sum_{l=1}^m \; R^{(re)}_l \otimes I_2 + R^{(im)}_l \otimes J~ \in \mathbb{R}^{2n \times 2n}\\ & ~~ ~~ \text{with} \; R^{(re)}_{l,(k,k')} = \mathfrak{R}(\beta_{l,k}\bar{\beta}_{l,k'})\; \text{ and } \; R^{(im)}_{l,(k,k')} = \mathfrak{I}(\beta_{l,k}\bar{\beta}_{l,k'}) \; ; \\ & \tilde{J} = \mathbf{I}_n \otimes [0 \; ,\; 1 \; ;\; -1 \; ,\; 0 ] ~ \in \mathbb{R}^{2n \times 2n} \; ; \\ & \tilde\delta^{(j,j')} = \mathrm{diag}_k\left(\Delta_k + \frac{\chi_{j,k}+\chi_{j',k}}{2}\right) \otimes [0 \; ,\; 1 \; ;\; -1 \; ,\; 0 ] ~ \in \mathbb{R}^{2n \times 2n} \; ; \\ & \tilde\omega^{(j,j')} = -i\, \mathrm{diag}_k \left( \frac{\chi_{j,k}-\chi_{j',k}}{2} \right) \otimes \mathbf{I}_2 ~ \in \mathbb{C}^{2n \times 2n}\; ; \\ & \beta_{l,A} = [\mathfrak{R}(\beta_{l,1});\; -\mathfrak{I}(\beta_{l,1});\; \mathfrak{R}(\beta_{l,2});\; -\mathfrak{I}(\beta_{l,2});\; ... ] ~ \in \mathbb{R}^{2n} \; ; \\ & B = \sum_{l=1}^m \; \eta_l \beta_{l,A} \, \beta_{l,A}^\dagger ~ \in \mathbb{R}^{2n \times 2n} \; , \end{align*} \]

the Gaussian kernels \( K^{(j,j')}_{t}(q,q_0)\) contain the following variables with purely deterministic evolution:

\[ \begin{eqnarray} \tfrac{d}{dt} S_t^{(j,j')} &=& [\tilde{\delta}^{(j,j')},\, S^{(j,j')}_t] - \tfrac{1}{2} \{ \tilde{R},\, S^{(j,j')}_t\} + \tfrac{1}{2} (\tilde{R}-\tilde{\omega}^{(j,j')}) \end{eqnarray} \]

(66)

\[ \begin{eqnarray} && + 2 S^{(j,j')}_t\, \tilde\omega^{(j,j')}\, S^{(j,j')}_t - 2 (S^{(j,j')}_t - \tfrac{\mathbf{I}_{2n}}{2}) \, B\, (S^{(j,j')}_t - \tfrac{\mathbf{I}_{2n}}{2}) \; ,\\ \tfrac{d}{dt} M^{(j,j')}_t &=& \left(\, \tilde{\delta}^{(j,j')} + 2 S^{(j,j')}_t \, \tilde{\omega}^{(j,j')} - \tfrac{1}{2} \tilde{R} - 2 (S^{(j,j')}_t - \tfrac{\mathbf{I}_{2n}}{2})\, B \right) \, M^{(j,j')}_t \; ,\\ \tfrac{d}{dt} D_t &=& 2 \bar{M}^\dagger_t\, \tilde{\omega}\, M_t - 2 \bar{M}^\dagger_t\, B \, M_t \; , \\\end{eqnarray} \]

initialized with \( S^{(j,j')}_0=D^{(j,j')}_0=\mathbf{0}_{2n}\) and \( M^{(j,j')}_0 = \mathbf{I}_{2n}\) .
It features the following independent stochastic variables:

\[ \begin{eqnarray} d\gamma^{(j=j')}_t &=& \tilde{J}\, u_t \, dt + \tilde{\delta}^{(j=j')} \, \gamma^{(j=j')}_t \, dt - \tfrac{1}{2} \tilde{R} \, \gamma^{(j=j')}_t \, dt \\ && - \, (S_t^{(j=j')}-\tfrac{\mathbf{I}_{2n}}{2})\, \left( 2\, B \gamma^{(j=j')}_t\, dt - {\textstyle \sum_{l=1}^m }\; \sqrt{\eta_l} \, \beta_{l,A} \, dy_{t,l} \right) \; ,\\ d\mu^{(j=j')}_{t} &=& 2 \, \mu^{(j=j')}_{t} \; \sum_{l=1}^m \, \sqrt{\eta_l}\, \beta_{l,A}^\dagger \left(\gamma^{(j=j')}_t - Q_{t}\right) \, \left( dy_{t,l} - 2 \sqrt{\eta_l}\, \beta_{l,A}^\dagger \, Q_{t} \; dt \right)\; , \\ \nonumber d(\mathrm{phase}(\mu_t^{(1,j')})) &=& 2 \sum_{l=1}^m \; \sqrt{\eta_l}\, \beta_{l,A}^\dagger\, \mathfrak{I}(\gamma^{(1,j')}_t) \; dy_{t,l} - 2 \mathfrak{I}\left((\bar{\gamma}^{(1,j')}_t)^\dagger \,(B-\tilde{\omega}^{(1,j')})\, \gamma^{(1,j')}_t \right) \, dt \\ && + \mathfrak{I}\left(\mathrm{Tr}\left( \tilde{\omega}^{(1,j')} \, (S^{(1,j')}_t - \tfrac{\mathbf{I}_{2n}}{2}) \right) \right) \, dt \; , \\\end{eqnarray} \]

initialized with \( \gamma^{(j,j')}_0=0\) and \( \mu_0^{(j,j')} = \text{Tr}(\rho_{0,(j,j')})\) , where the measurements give \( dy_{t,l} = 2 \sqrt{\eta_l}\, \beta_{l,A}^\dagger \, Q_{t} \; dt + dw_{t,l}\) and \( Q_{t} = [\,\text{Tr}(\rho_t\mathbf{X}_1);\;\text{Tr}(\rho_t\mathbf{P}_1);\;\text{Tr}(\rho_t\mathbf{X}_2);\;\text{Tr}(\rho_t\mathbf{P}_2);\;... \,] \; \in \mathbb{R}^{2n}\) .
The remaining variables are deterministically linked to those stochastic variables as follows:

\[ \begin{eqnarray} \lambda_t^{(j,j')} &=& 2 \bar{M}_t^{(j,j')\dagger}\,(\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j,j')})^{-1}\, (h_t^{(j,j')}- \gamma_t^{(j,j')}) \\ && \text{where}\\ \nonumber && \tfrac{d}{dt} h_t^{(j,j')} = \tilde{J} \, u_t + (\tilde{\delta}+\tilde{\omega}- \tfrac{\tilde{R}}{2})^{(j,j')} \, h_t^{(j,j')} \; , \\ \gamma_t^{(j,j')} &=& (\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j,j')}) \Bigg( \tilde{X}^{(j,j')}_t - C_1\, (\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j,j)})^{-1}\; \gamma_t^{(j,j)} - C_2\, (\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j',j')})^{-1}\, \gamma_t^{(j',j')} \Bigg) \; \nonumber \\ \nonumber && \text{where}\\ && \tfrac{d}{dt}\tilde{X}^{(j,j')}_t = C^{(j,j',1)}_0 \left(\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j,j)} \right)^{-1} \tilde{J}\, u_t \;+\; C^{(j,j',2)}_0 \, \left(\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j',j')} \right)^{-1} \tilde{J}\, u_t \\ \nonumber &&\phantom{\tfrac{d}{dt}\tilde{X}^{(j,j')}_t = k} + \left(\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j,j')} \right)^{-1} \tilde{J}\, u_t \; +\;\; (\tilde{\delta}-\tilde{\omega}+ \tfrac{\tilde{R}}{2})^{(j,j')} \, \tilde{X}^{(j,j')}_t \; , \\ \log(|\mu_t^{(j,j')}|) &=& Y^{(j,j')}_{R,t} + \tfrac{1}{2}(\log(\mu)+\Gamma)_t^{(j,j)} +\tfrac{1}{2}(\log(\mu)+\Gamma)_t^{(j',j')} - \mathfrak{R}(\Gamma_t^{(j,j')}) \\ \nonumber && \text{where } \Gamma_t = \bar{\gamma}_t^\dagger \, (\tfrac{\mathbf{I}_{2n}}{2}-S_t^{(j,j)})^{-1}\, \gamma_t \; \text{ and }\\ \nonumber && \tfrac{d}{dt} Y^{(j,j')}_{R,t} = \frac{1}{2}\, \text{Tr}\left( B\, (S^{(j,j)}_t-\tfrac{\mathbf{I}_{2n}}{2} + S^{(j',j')}_t - \tfrac{\mathbf{I}_{2n}}{2})\, \right) \\ && \phantom{\tfrac{d}{dt} Y^{(j,j')}_{R,t} = k} + \mathfrak{R}\left(\, 2(\tilde{X}_t^{(j,j')})^\dagger \, \tilde{J} \, u_t - \text{Tr}\left( \,(B-\tilde{\omega}^{(j,j')})\,(S^{(j,j')}_t-\tfrac{\mathbf{I}_{2n}}{2})\, \right) \,\right) \; , \\ \mathrm{phase}(\mu_t^{(j,j')}) &=& Y^{(j,j',1)}_{I,t} + \mathrm{phase}(\mu_t^{(1,j')})- \mathrm{phase}(\mu_t^{(1,j)}) -\mathfrak{I}(\Gamma_t^{(j',1)}+\Gamma_t^{(1,j)}+\Gamma_t^{(j,j')}) \\ \nonumber && \text{where}\\ \nonumber && \nonumber \tfrac{d}{dt}\, Y^{(j,j',1)}_{I,t} = \mathfrak{I}\left(\, \text{Tr}\left( \,(B-\tilde{\omega}^{(j,j')})\, (\tfrac{\mathbf{I}_{2n}}{2}-S^{(j,j')}_t)\, \right) \,\right)\\ \nonumber && \phantom{\tfrac{d}{dt}\, Y^{}_{I,t}} + \mathfrak{I}\left(\, \text{Tr}\left( \,(B-\tilde{\omega}^{(j',1)})\, (\tfrac{\mathbf{I}_{2n}}{2}-S^{(j',1)}_t) + (B-\tilde{\omega}^{(1,j)})\, (\tfrac{\mathbf{I}_{2n}}{2}-S^{(1,j)}_t)\, \right) \,\right)\\ \nonumber && \phantom{\tfrac{d}{dt}\, Y^{}_{I,t}} + 2 \, \mathfrak{I}(\tilde{X}^{(j,j')}_t + \tilde{X}^{(j',1)}_t + \tilde{X}^{(1,j)}_t )^\dagger \, \tilde{J} \, u_t \, , \\\end{eqnarray} \]

with \( C_1 = -\mathbf{I}_{2n}/2 + i\,\tilde{J}/2\) and \( C_2 = -\mathbf{I}_{2n}/2 - i\,\tilde{J}/2\) , and with the initialization:

\[ \begin{eqnarray*} h_0^{(j,j')} = 0 \; , ~ \tilde{X}^{(j,j')}_0 = 0 \; , ~ Y^{(j,j')}_{R,0} = \log\left(\tfrac{|\mu_0^{(j,j')}|}{\sqrt{\mu_0^{(j,j)}\mu_0^{(j',j')} }}\right) \; , ~ Y^{(j,j',1)}_{I,0} = \mathrm{phase}\left(\tfrac{\mu_0^{(j,j')}\mu_0^{(1,j,)}}{\mu_0^{(1,j')}} \right) \; . \end{eqnarray*} \]

Specializing these to a single cavity with \( B = \eta\, \mathbf{I}_{2n}\) and \( \tilde{R}=2\, \mathbf{I}_{2n}\) (and \( \Delta_k=0\) ) yields back the differential equations behind the solutions of Proposition 11. Some of the above expressions are undefined when \( S_t - \mathbf{I}_{2n}\, /2\) becomes singular; the reader is invited to go back through the derivations above in order to smoothen out these points.

Note that each \( R_l^{(re)}\) above is positive semidefinite, while \( q^\dagger (R_l^{(im)}\otimes J) \, q = \overline{q^\dagger (R_l^{(im)\dagger}\otimes J^\dagger) \, q } = \overline{q^\dagger (R_l^{(im)}\otimes (-J)) q}= -q^\dagger (R_l^{(im)}\otimes J) \, q = 0\) , proving that \( \tilde{R}\) is positive semi-definite. It governs the rate at which \( S_t\) converges towards \( \mathbf{I}_{2n}\, /2\) and \( M_t\) converges towards \( \mathbf{0}_{2n}\) .

Assuming that this has happened (e.g. \( \tilde{R}\) positive definite), the Gaussian kernel factorizes into a function of \( q_0\) and a Gaussian in \( q\) . The former integrates out with the initial state as a constant, and the former expresses the product of coherent states towards which the cavity has converged, indexed by \( j,j'\) . In this limit, from (53), the \( \gamma^{(j',j)}\) undergo no stochastic motion anymore: they follow deterministic dynamics which depend on \( (j,j')\) but not on the measurement results (nor, consistently, on the \( \eta_l\) ). These correspond to the coherent state amplitudes. The \( D^{(j,j')}\) and the \( \lambda^{(j,j')}\) (see (61) to resolve the undefiniteness) don't vary anymore either and the relative weight \( \text{Tr}(\rho_{t,(j,j)})\) of qudit level \( j\) is governed by \( \mu_{t}^{(j,j)}\) . Like for the single oscillator case, we can note \( \tilde{\mu}_{t}^{(j,j)} = \text{Tr}(\rho_{t,(j,j)})\) with \( \tfrac{d\tilde{\mu}}{\tilde{\mu}} = \tfrac{d\mu}{\mu}\) , such that \( Q_t = \sum_{j'} \tilde{\mu}_t^{(j',j')} \, \gamma_t^{(j',j')}\) while \( \gamma_t^{(j,j)} = \gamma_t^{(j,j)} \, \sum_{j'} \tilde{\mu}_t^{(j',j')}\) . From these observations, we obtain:

\[ d\tilde{\mu}_t^{(j,j)} = 2 \, \tilde{\mu}_t^{(j,j)} \, \sum_{l=1}^m \, \sqrt{\eta_l} \, \beta_{l,A}^\dagger \, \left(\sum_{j'=1}^d \, ( \gamma_t^{(j,j)}- \gamma_t^{(j',j')})\, \tilde{\mu}_t^{(j',j')} \right) \, dw_{t,l} \; . \]

This generalization of (27) again matches the form (9). It expresses how the setting has become equivalent, in the limit, to a direct QND measurement of the \( \tilde{\mu}_t^{(j,j)}\) , with measurement operators \( L_l(t) = \sum_{j=1}^d \, |j\rangle\langle j|\,(\beta_{l,A}^\dagger \gamma_t^{(j,j)})\) .

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