This paper was converted on www.awesomepapers.org from LaTeX by an anonymous user.
Want to know more? Visit the Converter page.

Quantum dynamics under simultaneous and continuous measurement of noncommutative observables

Chao Jiang [email protected] Department of Physics and Zhejiang Institute of Modern Physics, Zhejiang University, Hangzhou, Zhejiang 310027, China    Gentaro Watanabe [email protected] Department of Physics and Zhejiang Institute of Modern Physics, Zhejiang University, Hangzhou, Zhejiang 310027, China Zhejiang Province Key Laboratory of Quantum Technology and Device, Zhejiang University, Hangzhou, Zhejiang 310027, China
Abstract

We consider simultaneous and continuous measurement of two noncommutative observables of the system whose commutator is not necessarily a cc-number. We revisit the Arthurs-Kelly model and generalize it to describe the simultaneous measurement of two observables of the system. Using this generalized model, we continuously measure the system by following the scheme proposed by Scott and Milburn [Scott and Milburn, Phys. Rev. A 63, 042101 (2001)]. We find that the unconditioned master equation reduces to the Lindblad form in the continuous limit. In addition, we find that the master equation does not contain a cross term of these two measurements. Finally, we propose a scheme to prepare the state of a two-level system in an external field by feedback control based on the simultaneous, continuous measurement of the two observables.

I Introduction

Quantum feedback control H. M. W. ; K. Jacobs2 ; H. M. Wiseman ; Diosi94 ; S. Lloyd ; Daniel ; Sagawa ; Brif is a widely employed technique to drive a quantum system to a desired state Bushev ; Dotsenko ; Gillett ; Vijay . Using measurement results to control system parameters, the feedback control technique provides a robust way to prepare the target state without fine tuning the protocol. The first application of quantum feedback control dates back to a scheme proposed by Yamamoto and his collaborators to produce an amplitude-squeezed state Yamamoto1 ; Yamamoto2 . In the recent decades, the development of cavity quantum electrodynamics (cavity QED) J. M. Raimond ; H. Mabuchi ; A. Blais and circuit quantum electrodynamics (cQED) based on superconducting qubits A. Wallraff ; J. Clarke has offered a promising platform for quantum information and computation. As a consequence, feedback control technology finds a broad application in the new field such as qubit resetting D. Riste1 , state stabilization C. Sayrin , quantum error correction J. Cramer , entanglement enhancement D. Riste2 , etc.

In the standard protocol of feedback control of a quantum system, continuous measurement V. B. Braginsky ; T. A. Brun ; K. Jacobs ; H. M. W. ; K. Jacobs2 ; A. A. Clerk is performed and the state of the system is manipulated in parallel according to the measurement outcome. Continuous measurement can be realized by coupling the system to an auxiliary system working as a measurement apparatus. By continuously interacting with the system, the state of the apparatus is influenced by the system, and hence the information of the system can be extracted continuously H.-P. Breuer ; H. M. W. ; K. Jacobs2 . If the coupling is weak enough and the apparatus does not have memory, i.e., the so-called Born-Markov approximation, the master equation of the system can be reduced to the celebrated Lindblad-Gorini-Kossakowski-Sudarshan form (in short, Lindblad form hereafter) H.-P. Breuer ; H. M. W. ; K. Jacobs2 ; Lindblad ; Gorini76 ; Carmichael .

Continuous measurement of a single observable has already been discussed in many works Barchielle ; N. Gisin ; C. M. Caves ; L. Diosi ; Presilla ; A. Steck ; J. Combes ; T. Konrad ; C. Laflamme ; Yang , and the feedback control theory based on the single-observable measurement is well established A. C. Doherty1 ; A. C. Doherty2 . On the other hand, as for simultaneous and continuous measurement of multiple observables, there is another fundamental issue when two noncommutative observables are simultaneously measured. Although several works have discussed the simultaneous, continuous measurement of two noncommutative observables, they either consider two particular observables, such as canonically conjugate variables A. J. Scott ; Gough ; Ochoa (i.e., the commutator of them is a cc-number) and qubit observables Chantasri ; Luis ; Shay , or assume that the system under the simultaneous and continuous measurement evolves according to the Lindblad form master equation without additional cross terms, which describe the interplay effect of the two individual measurements, even though the measured observables are not commutative K. Jacobs2 ; Chantasri ; A. Levy . In the present paper, instead of assuming, we will derive the master equation of the system under the simultaneous, continuous measurement of two arbitrary noncommutative observables, whose commutator is not a cc-number but an operator. We will start from a concrete measurement model, which can be used to describe the simultaneous and continuous measurement of two arbitrary observables, and show that the master equation obtained for simultaneous and continuous measurement of two observables whose commutator is a cc-number A. J. Scott is still valid regardless of the observables to be measured.

State preparation of qubits L. DiCarlo ; C. Song ; N. Friis ; T. L. Patti has always been a crucial issue in quantum information processing and quantum computation. This issue becomes more practically important in the current situation in which the recent development of cavity QED and cQED has spurred the fabrication of quantum computers. In addition, regarding our current problem, the angular momentum operators in a two-level system (TLS) of the qubit [i.e., spin-1/21/2 operators] are one of the simplest but nontrivial examples of observables whose commutator is not a cc-number. Among various techniques, the feedback control is a promising scheme that allows us to control the qubit state in a robust manner. Further, feedback control using the measurement outcome of two observables instead of one provides us with a more flexible way to control the system. Therefore, preparation of a designated target state of a TLS based on the simultaneous, continuous measurement of two noncommutative observables is a challenging but important task.

In this paper, we derive the unconditioned and conditioned master equations of the system under the continuous and simultaneous measurement, and we also provide a state preparation scheme for a TLS using a static external field, simultaneous and continuous measurement, and feedback control as an application of our formalism. First, we generalize the Arthurs-Kelly measurement model E. Arthurs ; S. L. Braunstein ; A. J. Scott to the simultaneous measurement of two arbitrary observables of the system. We show that the measurement outcome deviates from the true expectation value of the measured variables unless the coupling strengths between the system and the two detectors are sufficiently weak. This is a striking difference from the case where the commutator of the two observables is a cc-number. Following the method by Scott and Milburn A. J. Scott , we use this generalized model to describe the continuous measurement of two arbitrary observables, and derive both unconditioned and conditioned master equations. We find that the former can be reduced to the Lindblad form in the continuous limit, even if the coupling constant between the system and the apparatus is not infinitesimally small. Finally, using the obtained master equations, we discuss the state preparation of a spin-1/21/2 system by the feedback control based on the simultaneous, continuous measurement of different components of the spin. In our scheme, a target state is obtained as an asymptotic steady state of the time evolution. We find that the effect of measurement and feedback together on the resulting steady state is equivalent to a heat bath, which is similar to the harmonic oscillator case A. Levy , and we also derive analytical expressions of the timescale required to reach the steady state. Moreover, the static external magnetic field can generate coherence between the ground state and the excited state. Because of this property, the static external field together with the measurement and feedback control can be utilized to manipulate the state of a TLS in a versatile manner.

This paper is organized as follows. In Sec. II.1, we generalize the Arthurs-Kelly measurement model E. Arthurs ; S. L. Braunstein ; A. J. Scott and calculate the average and the variance of the measurement readout. In Sec. II.2, we simultaneously and continuously measure the system based on this generalized model. The unconditioned and the conditioned master equations are given in this section. In Sec. III, we perform measurement and feedback control on a TLS in an external magnetic field. Focusing on an asymptotic steady state of the system, we discuss effects of the external field, the measurement, and the feedback control. The summary and conclusion are given in Sec. IV.

II Measurement model

II.1 Generalization of Arthurs-Kelly measurement model

The Arthurs-Kelly model is a single-shot measurement model which can be used to describe the simultaneous measurement of the position and the momentum of a particle in a one-dimensional quantum system E. Arthurs ; S. L. Braunstein ; A. J. Scott . It consists of two detectors and the system to be measured. The pointers of the two detectors are prepared in the Gaussian initial state, and, at an instance of time trt_{r}, the position x^\hat{x} and the momentum p^\hat{p} of the particle are coupled with the pointers of the two detectors, respectively, when the measurement starts. After the coupling at trt_{r}, the positions of the two pointers are influenced by the system; therefore, we can obtain measured values of x^\hat{x} and p^\hat{p} from the readouts of the positions of the two pointers by projective measurements of their positions. The coupling between the system and the detectors is described by the time-dependent Hamiltonian H^I(t)\hat{H}_{I}(t), which is chosen in the following form:

H^I(t)=(s1x^p^1+s2p^p^2)δ(ttr),\displaystyle\hat{H}_{I}(t)=(s_{1}\hat{x}\hat{p}_{1}+s_{2}\hat{p}\hat{p}_{2})\,\delta(t-t_{r}), (1)

where p^i\hat{p}_{i} (i=1, 2)(i=1,\,2) is the momentum of detector ii’s pointer, sis_{i} is the coupling strength between the system and detector ii, and all the quantities here (i.e., H^I\hat{H}_{I}, sis_{i}, x^\hat{x}, p^\hat{p}, and p^i\hat{p}_{i}) are dimensionless.

We now consider simultaneous measurements of two arbitrary observables A^\hat{A} and B^\hat{B} of the system. This generalized measurement can be performed by the following analogical interaction Hamiltonian between the system and two detectors:

H^I(t)\displaystyle\hat{H}_{I}(t) =(s1A^p^1+s2B^p^2)δ(ttr).\displaystyle=(s_{1}\hat{A}\hat{p}_{1}+s_{2}\hat{B}\hat{p}_{2})\,\delta(t-t_{r}). (2)

Similarly, all the physical quantities discussed here such as H^I\hat{H}_{I}, sis_{i}, and A^\hat{A} are also dimensionless. Moreover, \hbar is set to be unity throughout the whole paper for simplicity note:units . Again, detector ii is still prepared in the Gaussian initial state |di\ket{d_{i}},

xi|di=(πΔi)1/4exp(xi22Δi),\displaystyle\left\langle x_{i}|d_{i}\right\rangle=(\pi\Delta_{i})^{-1/4}\,\exp{\left(-\frac{x_{i}^{2}}{2\Delta_{i}}\right)}, (3)

where |xi\ket{x_{i}} is the position eigenstate of detector ii’s pointer, Δisiσ2\Delta_{i}\equiv s_{i}\sigma^{2} (with si>0)(\textrm{with }s_{i}>0), and σ2\sigma^{2} is a parameter characterizing the measurement accuracy.

Before the coupling at trt_{r}, the system and the two detectors are assumed to be uncorrelated with each other. Therefore, the density operator of the total system including the system and the detectors initially takes the following form:

ρ^Tρ^s|d1d2d1d2|,\displaystyle\hat{\rho}_{T}\equiv\hat{\rho}_{s}\otimes|d_{1}d_{2}\rangle\langle d_{1}d_{2}|, (4)

where ρ^s\hat{\rho}_{s} is the partial density operator of the system and |d1d2|d1|d2|d_{1}d_{2}\rangle\equiv|d_{1}\rangle\otimes|d_{2}\rangle is the uncorrelated Gaussian initial state of two detectors.

After the coupling between the system and the detectors, the total system is in the state

ρ^T=U^Iρ^TU^I,\displaystyle\hat{\rho}_{T}^{\prime}=\hat{U}_{I}\hat{\rho}_{T}\hat{U}_{I}^{\dagger}, (5)

where

U^Iexp[i(s1A^p^1+s2B^p^2)]\displaystyle\hat{U}_{I}\equiv\exp\left[-i(s_{1}\hat{A}\hat{p}_{1}+s_{2}\hat{B}\hat{p}_{2})\right] (6)

is the evolution operator during the measurement. As a result, the average of observable A^\hat{A} and the position of the pointer of detector 1 after the coupling are given as

A^\displaystyle\left\langle\hat{A}\right\rangle^{\prime} =Tr(A^ρ^T)=Tr(U^IA^U^Iρ^T)U^IA^U^I,\displaystyle=\mathrm{Tr}\,(\hat{A}\hat{\rho}_{T}^{\prime})=\mathrm{Tr}\,(\hat{U}_{I}^{\dagger}\hat{A}\hat{U}_{I}\hat{\rho}_{T})\equiv\left\langle\hat{U}_{I}^{\dagger}\hat{A}\hat{U}_{I}\right\rangle, (7)
x^1\displaystyle\left\langle\hat{x}_{1}\right\rangle^{\prime} =Tr(x^1ρ^T)=Tr(U^Ix^1U^Iρ^T)U^Ix^1U^I.\displaystyle=\mathrm{Tr}\,(\hat{x}_{1}\hat{\rho}_{T}^{\prime})=\mathrm{Tr}\,(\hat{U}_{I}^{\dagger}\hat{x}_{1}\hat{U}_{I}\hat{\rho}_{T})\equiv\left\langle\hat{U}_{I}^{\dagger}\hat{x}_{1}\hat{U}_{I}\right\rangle. (8)

Applying the Baker-Campbell-Hausdorff relation to these two equations, we get

A^=A^s24σ2[B^,[B^,A^]]+O(si2σ4),\displaystyle\left\langle\hat{A}\right\rangle^{\prime}=\left\langle\hat{A}\right\rangle-\frac{s_{2}}{4\sigma^{2}}\left\langle[\hat{B},[\hat{B},\hat{A}]]\right\rangle+O\left(\frac{s_{i}^{2}}{\sigma^{4}}\right), (9)

and

x^1=s1[A^s212σ2[B^,[B^,A^]]+O(si2σ4)].\displaystyle\left\langle\hat{x}_{1}\right\rangle^{\prime}=s_{1}\left[\left\langle\hat{A}\right\rangle-\frac{s_{2}}{12\sigma^{2}}\left\langle[\hat{B},[\hat{B},\hat{A}]]\right\rangle+O\left(\frac{s_{i}^{2}}{\sigma^{4}}\right)\right]. (10)

Here, we only have evenfold commutators since p^i2n+1=0\left\langle\hat{p}_{i}^{2n+1}\right\rangle=0 for the Gaussian state for non-negative integer nn. Following the same procedure for B^\hat{B} and x^2\hat{x}_{2}, we can obtain B\left\langle B\right\rangle^{\prime} and x2\left\langle x_{2}\right\rangle^{\prime},

B^=B^s14σ2[A^,[A^,B^]]+O(si2σ4),\displaystyle\left\langle\hat{B}\right\rangle^{\prime}=\left\langle\hat{B}\right\rangle-\frac{s_{1}}{4\sigma^{2}}\left\langle[\hat{A},[\hat{A},\hat{B}]]\right\rangle+O\left(\frac{s_{i}^{2}}{\sigma^{4}}\right), (11)

and

x^2=s2[B^s112σ2[A^,[A^,B^]]+O(si2σ4)].\displaystyle\left\langle\hat{x}_{2}\right\rangle^{\prime}=s_{2}\left[\left\langle\hat{B}\right\rangle-\frac{s_{1}}{12\sigma^{2}}\left\langle[\hat{A},[\hat{A},\hat{B}]]\right\rangle+O\left(\frac{s_{i}^{2}}{\sigma^{4}}\right)\right]. (12)

If [B^,[B^,A^]]=[A^,[A^,B^]]=0\left[\hat{B},\left[\hat{B},\hat{A}\right]\right]=\left[\hat{A},\left[\hat{A},\hat{B}\right]\right]=0, for instance A^=x^\hat{A}=\hat{x} and B^=p^\hat{B}=\hat{p}, then all the multifold commutators vanish so that we get A^=s11x^1\left\langle\hat{A}\right\rangle^{\prime}=s_{1}^{-1}\left\langle\hat{x}_{1}\right\rangle^{\prime} and B^=s21x^2\left\langle\hat{B}\right\rangle^{\prime}=s_{2}^{-1}\left\langle\hat{x}_{2}\right\rangle^{\prime}. However, for a general case in which [B^,[B^,A^]][\hat{B},[\hat{B},\hat{A}]] and [A^,[A^,B^]]\left[\hat{A},\left[\hat{A},\hat{B}\right]\right] are nonzero, all the higher-order terms remain and thus the measurement result si1x^is_{i}^{-1}\left\langle\hat{x}_{i}\right\rangle^{\prime} deviates from A^\left\langle\hat{A}\right\rangle^{\prime} and B^\left\langle\hat{B}\right\rangle^{\prime}. From Eqs. (9) – (12), we see that the leading order of the deviations is si/σ2s_{i}/\sigma^{2}, and thus the deviations are negligible only when si/σ21s_{i}/\sigma^{2}\ll 1. To discuss the deviations, it is convenient to introduce relative deviations ϵ1\epsilon_{1} and ϵ2\epsilon_{2} defined as

ϵ1\displaystyle\epsilon_{1} x^1s1A^s1A^,\displaystyle\equiv\frac{\left\langle\hat{x}_{1}\right\rangle^{\prime}-s_{1}\left\langle\hat{A}\right\rangle^{\prime}}{s_{1}\left\langle\hat{A}\right\rangle^{\prime}}, (13)
ϵ2\displaystyle\epsilon_{2} x^2s2B^s2B^.\displaystyle\equiv\frac{\left\langle\hat{x}_{2}\right\rangle^{\prime}-s_{2}\left\langle\hat{B}\right\rangle^{\prime}}{s_{2}\left\langle\hat{B}\right\rangle^{\prime}}. (14)

For A^=L^x\hat{A}=\hat{L}_{x} and B^=L^y\hat{B}=\hat{L}_{y} as an example, where L^x\hat{L}_{x} and L^y\hat{L}_{y} are xx and yy components of the angular momentum, respectively note:angularmom , ϵ1\epsilon_{1} and ϵ2\epsilon_{2}, with si1x^is_{i}^{-1}\left\langle\hat{x}_{i}\right\rangle^{\prime}, A^\left\langle\hat{A}\right\rangle^{\prime}, and B^\left\langle\hat{B}\right\rangle^{\prime} up to the second order of si/σ2s_{i}/\sigma^{2}, read

ϵ1\displaystyle\epsilon_{1} =s26σ21(s1+3s2)/20σ21s2/4σ2+s2(s1+3s2)/96σ4,\displaystyle=\frac{s_{2}}{6\sigma^{2}}\frac{1-(s_{1}+3s_{2})/20\sigma^{2}}{1-s_{2}/4\sigma^{2}+s_{2}(s_{1}+3s_{2})/96\sigma^{4}}, (15)
ϵ2\displaystyle\epsilon_{2} =s16σ21(s2+3s1)/20σ21s1/4σ2+s1(s2+3s1)/96σ4.\displaystyle=\frac{s_{1}}{6\sigma^{2}}\frac{1-(s_{2}+3s_{1})/20\sigma^{2}}{1-s_{1}/4\sigma^{2}+s_{1}(s_{2}+3s_{1})/96\sigma^{4}}. (16)

In Eqs. (15) and (16), ϵ1\epsilon_{1} and ϵ2\epsilon_{2} are independent of the state of the system due to the closed algebra of the angular momentum and the symmetry of the Gaussian state. Take ϵ1\epsilon_{1} for example: because of the closed algebra of the angular momentum, the numerator and the denominator of ϵ1\epsilon_{1} can be written as a linear combination of L^x\left\langle\hat{L}_{x}\right\rangle, L^y\left\langle\hat{L}_{y}\right\rangle, and L^z\left\langle\hat{L}_{z}\right\rangle. However, due to the symmetry of the Gaussian state, the coefficients of L^y\left\langle\hat{L}_{y}\right\rangle and L^z\left\langle\hat{L}_{z}\right\rangle, which are averages of odd powers of x^i\hat{x}_{i} and p^i\hat{p}_{i}, are zero. Therefore, the numerator and the denominator of ϵ1\epsilon_{1} are proportional to L^x\left\langle\hat{L}_{x}\right\rangle, which are canceled with each other finally. The relative deviations ϵ1\epsilon_{1} and ϵ2\epsilon_{2} are monotonically increasing with parameters s1/σ2s_{1}/\sigma^{2} and s2/σ2s_{2}/\sigma^{2}. When si/σ20.5s_{i}/\sigma^{2}\simeq 0.5, the relative deviations ϵ1\epsilon_{1} and ϵ2\epsilon_{2} reach around 10%10\%, which are non-negligible. Consequently, si/σ2s_{i}/\sigma^{2} must be much smaller than 1 in order to obtain an accurate measurement outcome. Details are shown in Fig. 1.

Refer to caption
Figure 1: Relative deviations (a) ϵ1\epsilon_{1} and (b) ϵ2\epsilon_{2} as functions of s1/σ2s_{1}/\sigma^{2} and s2/σ2s_{2}/\sigma^{2} for A^=L^x\hat{A}=\hat{L}_{x} and B^=L^y\hat{B}=\hat{L}_{y}. ϵ1\epsilon_{1} and ϵ2\epsilon_{2} are monotonically increasing functions of si/σ2s_{i}/\sigma^{2}.

We now go back to the arbitrary observables A^\hat{A} and B^\hat{B}, and consider the second moment of the positions of the two pointers x^1\hat{x}_{1} and x^2\hat{x}_{2} after the coupling,

x^12=\displaystyle\left\langle\hat{x}_{1}^{2}\right\rangle^{\prime}= s1σ22[1+2s1σ2A^2s1s212σ4([B^,[B^,A^2]]\displaystyle\frac{s_{1}\sigma^{2}}{2}\left[1+\frac{2s_{1}}{\sigma^{2}}\left\langle\hat{A}^{2}\right\rangle-\frac{s_{1}s_{2}}{12\sigma^{4}}\Big{(}\left\langle[\hat{B},[\hat{B},\hat{A}^{2}]]\right\rangle\right.
+A^[B^,[B^,A^]]+[B^,A^[B^,A^]])+O(si3σ6)],\displaystyle\left.+\left\langle\hat{A}\,[\hat{B},[\hat{B},\hat{A}]]\right\rangle+\left\langle[\hat{B},\hat{A}\,[\hat{B},\hat{A}]]\right\rangle\Big{)}+O\left(\frac{s_{i}^{3}}{\sigma^{6}}\right)\right], (17)

and

x^22=\displaystyle\left\langle\hat{x}_{2}^{2}\right\rangle^{\prime}= s2σ22[1+2s2σ2B^2s1s212σ4([A^,[A^,B^2]]\displaystyle\frac{s_{2}\sigma^{2}}{2}\left[1+\frac{2s_{2}}{\sigma^{2}}\left\langle\hat{B}^{2}\right\rangle-\frac{s_{1}s_{2}}{12\sigma^{4}}\Big{(}\left\langle[\hat{A},[\hat{A},\hat{B}^{2}]]\right\rangle\right.
+B^[A^,[A^,B^]]+[A^,B^[A^,B^]])+O(si3σ6)].\displaystyle\left.+\left\langle\hat{B}\,[\hat{A},[\hat{A},\hat{B}]]\right\rangle+\left\langle[\hat{A},\hat{B}\,[\hat{A},\hat{B}]]\right\rangle\Big{)}+O\left(\frac{s_{i}^{3}}{\sigma^{6}}\right)\right]. (18)

The leading term of the variance x^i2(x^i)2\left\langle\hat{x}_{i}^{2}\right\rangle^{\prime}-\left(\left\langle\hat{x}_{i}\right\rangle^{\prime}\right)^{2} of the measurement result depends on the parameter siσ2s_{i}\sigma^{2}. In order to get a stable readout, i.e., the variances are small so that the measurement results are less scattered, siσ2s_{i}\sigma^{2} need to be set as small as possible. There is a tradeoff between the stability characterized by siσ2s_{i}\sigma^{2} and the accuracy characterized by si/σ2s_{i}/\sigma^{2} [see Eqs. (15) and (16)]. Therefore, σ2\sigma^{2} cannot be too large for a given sis_{i}, although σ2\sigma^{2} is intrinsically a large quantity in the weak measurements, which is assumed to hold si/σ21s_{i}/\sigma^{2}\ll 1. On the other hand, for a given σ2\sigma^{2}, sis_{i} should be sufficiently small so that both siσ2s_{i}\sigma^{2} and si/σ2s_{i}/\sigma^{2} are smaller than unity. From this point of view, the generalized Arthurs-Kelly measurement model is valid only for a weak measurement.

II.2 Continuous measurement

A continuous and simultaneous measurement of observables A^\hat{A} and B^\hat{B} can be realized by the following interaction Hamiltonian A. J. Scott :

H^I(t)=n=1(s1A^p^1+s2B^p^2)δ(tnδt),\displaystyle\hat{H}_{I}(t)=\sum_{n=1}^{\infty}(s_{1}\hat{A}\hat{p}_{1}+s_{2}\hat{B}\hat{p}_{2})\,\delta(t-n\delta t), (19)

where δt\delta t is the time interval between two consecutive measurements and will finally be set to be infinitesimal. After each single-shot measurement, the readouts of x1x_{1} and x2x_{2} are recorded, and then the total composite system is reset to the decoupled initial state given by Eq. (4) based on the Born-Markov assumption. The state of the system immediately before and after the nnth measurement is denoted by ρ^s(nδt)\hat{\rho}_{s}(n\delta t) and ρ^s(nδt)\hat{\rho}_{s}^{\prime}(n\delta t) respectively, which satisfy the following relationship:

ρ^s(nδt)=Trd[U^Iρ^s(nδt)|d1d2d1d2|U^I],\displaystyle\hat{\rho}^{\prime}_{s}(n\delta t)=\mathrm{Tr}\,_{d}\left[\hat{U}_{I}\hat{\rho}_{s}(n\delta t)\otimes|d_{1}d_{2}\rangle\langle d_{1}d_{2}|\hat{U}_{I}^{\dagger}\right], (20)

where Trd\mathrm{Tr}\,_{d} means the trace over the degrees of freedom of the two detectors.

We introduce the following measurement operator:

M^(x1,x2)\displaystyle\hat{M}(x_{1},x_{2})\equiv x1x2|U^I|d1d2\displaystyle\left\langle x_{1}x_{2}|\hat{U}_{I}|d_{1}d_{2}\right\rangle
=\displaystyle= 𝑑p1𝑑p2x1x2|U^I|p1p2p1p2|d1d2\displaystyle\int dp_{1}dp_{2}\,\left\langle x_{1}x_{2}|\hat{U}_{I}|p_{1}p_{2}\right\rangle\left\langle p_{1}p_{2}|d_{1}d_{2}\right\rangle
=\displaystyle= (2π)1dp1dp2exp{i[(x1s1A^)p1\displaystyle(2\pi)^{-1}\int dp_{1}dp_{2}\ \exp\left\{i[(x_{1}-s_{1}\hat{A})p_{1}\right.
+(x2s2B^)p2]}p1p2|d1d2,\displaystyle\left.+(x_{2}-s_{2}\hat{B})p_{2}]\right\}\left\langle p_{1}p_{2}|d_{1}d_{2}\right\rangle, (21)

where |x1x2|x1|x2\ket{x_{1}x_{2}}\equiv\ket{x_{1}}\otimes\ket{x_{2}}, |p1p2|p1|p2\ket{p_{1}p_{2}}\equiv\ket{p_{1}}\otimes\ket{p_{2}}, and |pi\ket{p_{i}} is the eigenstate of the momentum of detector ii’s pointer. Equation (20) can be rewritten explicitly as

ρ^s(nδt)=\displaystyle\hat{\rho}^{\prime}_{s}(n\delta t)= 𝑑x1𝑑x2M^(x1,x2)ρ^s(nδt)M^(x1,x2)\displaystyle\int dx_{1}dx_{2}\ \hat{M}(x_{1},x_{2})\,\hat{\rho}_{s}(n\delta t)\,\hat{M}^{\dagger}(x_{1},x_{2})
=\displaystyle= 𝑑p1𝑑p2exp[i(s1p1A^+s2p2B^)]ρ^s(nδt)\displaystyle\int dp_{1}dp_{2}\ \exp\left[-i(s_{1}p_{1}\hat{A}+s_{2}p_{2}\hat{B})\right]\,\hat{\rho}_{s}(n\delta t)
exp[i(s1p1A^+s2p2B^)]|p1p2|d1d2|2\displaystyle\exp\left[i(s_{1}p_{1}\hat{A}+s_{2}p_{2}\hat{B})\right]\,\left|\left\langle p_{1}p_{2}|d_{1}d_{2}\right\rangle\right|^{2}
=\displaystyle= ρ^s(nδt)s14σ2[A^,[A^,ρ^s(nδt)]]\displaystyle\hat{\rho}_{s}(n\delta t)-\frac{s_{1}}{4\sigma^{2}}[\hat{A},[\hat{A},\hat{\rho}_{s}(n\delta t)]]
s24σ2[B^,[B^,ρ^s(nδt)]]+O(si2σ4).\displaystyle-\frac{s_{2}}{4\sigma^{2}}[\hat{B},[\hat{B},\hat{\rho}_{s}(n\delta t)]]+O\left(\frac{s_{i}^{2}}{\sigma^{4}}\right). (22)

Note that the right-hand side of the last equality of Eq. (22) contains neither the terms [A^,[B^,ρ^s]][\hat{A},[\hat{B},\hat{\rho}_{s}]] nor [B^,[A^,ρ^s]][\hat{B},[\hat{A},\hat{\rho}_{s}]], which describe the interplay effect between the measurements of the two observables, because their coefficients are zero for Gaussian states.

Taking the unitary evolution by the system Hamiltonian H^s\hat{H}_{s} after each measurement into consideration, the state of the system becomes

ρ^s(nδt+δt)=U^sρ^s(nδt)U^s,\displaystyle\hat{\rho}_{s}(n\delta t+\delta t)=\hat{U}_{s}\,\hat{\rho}^{\prime}_{s}(n\delta t)\,\hat{U}_{s}^{\dagger}, (23)

where

U^sexp(iH^sδt)\displaystyle\hat{U}_{s}\equiv\exp\left(-i\hat{H}_{s}\delta t\right) (24)

is the unitary evolution operator between two consecutive measurements. After taking the continuous limit δt0\delta t\to 0 and σ\sigma\to\infty with ζ1/(δtσ2)=const.\zeta\equiv 1/(\delta t\,\sigma^{2})=\mathrm{const.}, the unconditioned master equation of the system under the simultaneous and continuous measurement reduces to the Lindblad form H.-P. Breuer ; H. M. W. ; K. Jacobs2 ; Lindblad ; Gorini76 :

dρ^sdt=i[H^s,ρ^s]γ18[A^,[A^,ρ^s]]γ28[B^,[B^,ρ^s]].\displaystyle\frac{d\hat{\rho}_{s}}{dt}=-i[\hat{H}_{s},\hat{\rho}_{s}]-\frac{\gamma_{1}}{8}[\hat{A},[\hat{A},\hat{\rho}_{s}]]-\frac{\gamma_{2}}{8}[\hat{B},[\hat{B},\hat{\rho}_{s}]]. (25)

Here, γi2siζ\gamma_{i}\equiv 2s_{i}\zeta is the measurement strength of A^\hat{A} (i=1)(i=1) or B^\hat{B} (i=2)(i=2). In addition, we can obtain the master equation for the measurement of a single observable A^\hat{A} or B^\hat{B} by setting s2s_{2} or s1s_{1} to be zero, respectively. Note that even for noninfinitesimal sis_{i}, the master equation (25) for simultaneous and continuous measurement is still valid in the continuous limit si/σ20s_{i}/\sigma^{2}\to 0, unlike the results for the single-shot measurement in the previous section.

The final master equation (25) of simultaneous measurement does not contain terms of the interplay effect such as [A^,[B^,ρ^s]][\hat{A},[\hat{B},\hat{\rho}_{s}]] and [B^,[A^,ρ^s]][\hat{B},[\hat{A},\hat{\rho}_{s}]], but just consists of a linear combination of the two independent measurement effects. This is because of the uncorrelated Gaussian initial state and the Born-Markovian approximation: Before each single-shot measurement, the total composite system is reset to the decoupled initial state given by Eq. (4). In addition, according to Eq. (22), the single-shot measurement discussed in the previous section does not introduce the terms of the interplay effect in the master equation if the initial state of the system and the two detectors are uncorrelated with each other and the detectors are initially prepared in the Gaussian state. Therefore, the terms of the interplay effects [A^,[B^,ρ^s]][\hat{A},[\hat{B},\hat{\rho}_{s}]] and [B^,[A^,ρ^s]][\hat{B},[\hat{A},\hat{\rho}_{s}]] are absent in the final master equation. Note that for A^=x^\hat{A}=\hat{x} and B^=p^\hat{B}=\hat{p} considered in Ref. A. J. Scott , such terms of the interplay effect have vanished, [x^,[p^,ρ^s]][p^,[x^,ρ^s]]=0[\hat{x},[\hat{p},\hat{\rho}_{s}]]-[\hat{p},[\hat{x},\hat{\rho}_{s}]]=0, because of [x^,p^]=i[\hat{x},\hat{p}]=i. Thus, even though the master equation of the simultaneous and continuous measurement of x^\hat{x} and p^\hat{p} does not contain the terms of the interplay effect of the two measurements A. J. Scott , it is still open whether this equation still holds for arbitrary observables A^\hat{A} and B^\hat{B}. Here, we have shown that the master equation indeed does not contain the terms of the interplay effect, irrespective of the observables measured.

Moreover, we shall also derive the conditioned master equation of simultaneous measurement. The nnth measurement outcome of detector ii is denoted by xi(n)x_{i}(n) and the final master equation is conditioned by a sequence of the outcome {xi(n)}\{x_{i}(n)\}. The average and the variance of xi(n)x_{i}(n) can be obtained by keeping the leading terms of Eqs. (10), (12), (17), and (18),

E[x1(n)]\displaystyle E\left[x_{1}(n)\right] s1A^,\displaystyle\approx s_{1}\left\langle\hat{A}\right\rangle, (26)
E[x2(n)]\displaystyle E\left[x_{2}(n)\right] s2B^,\displaystyle\approx s_{2}\left\langle\hat{B}\right\rangle, (27)
V[xi(n)]\displaystyle V\left[x_{i}(n)\right] =x^i2(x^i)2si2ζδt,\displaystyle=\left\langle\hat{x}_{i}^{2}\right\rangle^{\prime}-\left(\left\langle\hat{x}_{i}\right\rangle^{\prime}\right)^{2}\approx\frac{s_{i}}{2\zeta\delta t}, (28)

where E[]E[\cdots] represents the ensemble average over all the experimental realizations and V[]V[\cdots] represents the variance of the measurement outcome. The correlation function of x^1\hat{x}_{1} and x^2\hat{x}_{2} after the coupling can also be obtained:

x^1x^2=\displaystyle\left\langle\hat{x}_{1}\hat{x}_{2}\right\rangle^{\prime}= Tr(x^1x^2ρ^T)\displaystyle\mathrm{Tr}\,\left(\hat{x}_{1}\hat{x}_{2}\hat{\rho}_{T}^{\prime}\right)
=\displaystyle= s1s22A^B^+B^A^.\displaystyle\frac{s_{1}s_{2}}{2}\left\langle\hat{A}\hat{B}+\hat{B}\hat{A}\right\rangle. (29)

Comparing Eqs. (28) and (29), we find the covariance C[x1(n),x2(n)]x^1x^2x^1x^2C[x_{1}(n),x_{2}(n)]\equiv\langle\hat{x}_{1}\hat{x}_{2}\rangle^{\prime}-\langle\hat{x}_{1}\rangle^{\prime}\langle\hat{x}_{2}\rangle^{\prime} of x^1\hat{x}_{1} and x^2\hat{x}_{2} [which is of the order of (δt)0(\delta t)^{0}] is much smaller than the variance of x^1\hat{x}_{1} and x^2\hat{x}_{2} (which is of the order of 1/δt1/\delta t) in the continuous limit δt0\delta t\to 0. Therefore, the correlation between x^1\hat{x}_{1} and x^2\hat{x}_{2} can be neglected within the current approximation where the terms of order 1/δt1/\delta t are kept for the second moment of xix_{i}, and x1(n)x_{1}(n) and x2(n)x_{2}(n) can be treated as two uncorrelated random variables note:covar . Then, approximating xi(n)x_{i}(n) as a Gaussian random variable, xi(n)x_{i}(n) can be written as a summation of its average and fluctuation,

x1(n)\displaystyle x_{1}(n) =s1A^+s12ζdξ1(n)(δt)1\displaystyle=s_{1}\left\langle\hat{A}\right\rangle+\sqrt{\frac{s_{1}}{2\zeta}}\,d\xi_{1}(n)\cdot(\delta t)^{-1}
s1A^+λ1dξ1(n)(δt)1,\displaystyle\equiv s_{1}\left\langle\hat{A}\right\rangle+\lambda_{1}\,d\xi_{1}(n)\cdot(\delta t)^{-1}, (30)

and

x2(n)\displaystyle x_{2}(n) =s2B^+s22ζdξ2(n)(δt)1\displaystyle=s_{2}\left\langle\hat{B}\right\rangle+\sqrt{\frac{s_{2}}{2\zeta}}\,d\xi_{2}(n)\cdot(\delta t)^{-1}
s2B^+λ2dξ2(n)(δt)1,\displaystyle\equiv s_{2}\left\langle\hat{B}\right\rangle+\lambda_{2}\,d\xi_{2}(n)\cdot(\delta t)^{-1}, (31)

where λisi/2ζ\lambda_{i}\equiv\sqrt{s_{i}/2\zeta} is the fluctuation of the measurement outcome of observables A^\hat{A} (i=1i=1) and B^\hat{B} (i=2i=2), and dξid\xi_{i} is the Itô increment C. W. ; N. G. V. Kampen which satisfies

E[dξi]=0,\displaystyle E[d\xi_{i}]=0, (32)
E[dξi(m)dξi(n)]=δmnδt,\displaystyle E[d\xi_{i}(m)\cdot d\xi_{i}(n)]=\delta_{mn}\cdot\delta t, (33)
E[dξ1(n)dξ2(n)]=0.\displaystyle E[d\xi_{1}(n)\cdot d\xi_{2}(n)]=0. (34)

For notational simplicity, we will treat dξid\xi_{i} to be equal to δt1/2\delta t^{1/2} and omit the symbol E[]E[\cdots] in the following derivation. Then, the measurement operator can be expanded as

M^(x1(n),x2(n))=\displaystyle\hat{M}(x_{1}(n),x_{2}(n))= (2π)1𝑑p1𝑑p2exp{i[x1(n)p1+x2(n)p2]}exp[i(s1p1A^+s2p2B^)]\displaystyle(2\pi)^{-1}\int dp_{1}dp_{2}\ \exp\left\{i[x_{1}(n)p_{1}+x_{2}(n)p_{2}]\right\}\exp\left[-i(s_{1}p_{1}\hat{A}+s_{2}p_{2}\hat{B})\right]
(Δ1Δ2)1/4π1/2exp(Δ1p12+Δ2p222)\displaystyle\cdot\frac{(\Delta_{1}\Delta_{2})^{-1/4}}{\pi^{1/2}}\exp\left(-\frac{\Delta_{1}p_{1}^{2}+\Delta_{2}p_{2}^{2}}{2}\right)
\displaystyle\propto 𝑑p1𝑑p2exp{i(s1p1A^+s2p2B^)}exp[Δ1(p1ix1(n)Δ1)2+Δ2(p2ix2(n)Δ2)22]\displaystyle\int dp_{1}dp_{2}\ \exp\left\{-i(s_{1}p_{1}\hat{A}+s_{2}p_{2}\hat{B})\right\}\exp\left[-\frac{\Delta_{1}\left(p_{1}-\frac{ix_{1}(n)}{\Delta_{1}}\right)^{2}+\Delta_{2}\left(p_{2}-\frac{ix_{2}(n)}{\Delta_{2}}\right)^{2}}{2}\right]
=\displaystyle= 𝑑p1𝑑p2{n=01n![i(s1p1A^+s2p2B^)]n}exp[Δ1(p1ix1(n)Δ1)2+Δ2(p2ix2(n)Δ2)22]\displaystyle\int dp_{1}dp_{2}\ \left\{\sum_{n=0}^{\infty}\frac{1}{n!}\left[-i(s_{1}p_{1}\hat{A}+s_{2}p_{2}\hat{B})\right]^{n}\right\}\cdot\exp\left[-\frac{\Delta_{1}\left(p_{1}-\frac{ix_{1}(n)}{\Delta_{1}}\right)^{2}+\Delta_{2}\left(p_{2}-\frac{ix_{2}(n)}{\Delta_{2}}\right)^{2}}{2}\right]
=\displaystyle= 2π(Δ1Δ2)1/2[1+s1A^Δ1x1(n)+s2B^Δ2x2(n)s12A^22Δ1+s12A^22Δ12x1(n)2s22B^22Δ2+s22B^22Δ22x2(n)2]+O(δt3/2)\displaystyle\ \frac{2\pi}{(\Delta_{1}\Delta_{2})^{1/2}}\bigg{[}1+\frac{s_{1}\hat{A}}{\Delta_{1}}x_{1}(n)+\frac{s_{2}\hat{B}}{\Delta_{2}}x_{2}(n)-\frac{s_{1}^{2}\hat{A}^{2}}{2\Delta_{1}}+\frac{s_{1}^{2}\hat{A}^{2}}{2\Delta_{1}^{2}}x_{1}(n)^{2}-\frac{s_{2}^{2}\hat{B}^{2}}{2\Delta_{2}}+\frac{s_{2}^{2}\hat{B}^{2}}{2\Delta_{2}^{2}}x_{2}(n)^{2}\bigg{]}+O\left(\delta t^{3/2}\right)
\displaystyle\propto 1+ζδt(s1A^A^+s2B^B^s1A^24s2B^24)+λ1ζA^dξ1+λ2ζB^dξ2+O(δt3/2).\displaystyle\ 1+\zeta\delta t\left(s_{1}\left\langle\hat{A}\right\rangle\hat{A}+s_{2}\left\langle\hat{B}\right\rangle\hat{B}-\frac{s_{1}\hat{A}^{2}}{4}-\frac{s_{2}\hat{B}^{2}}{4}\right)+\lambda_{1}\zeta\,\hat{A}\,d\xi_{1}+\lambda_{2}\zeta\,\hat{B}\,d\xi_{2}+O\left(\delta t^{3/2}\right). (35)

The unnormalized state of the system after monitoring then becomes

ρ^s(nδt)=\displaystyle\hat{\rho}^{\prime}_{s}(n\delta t)= M^ρ^s(nδt)M^\displaystyle\hat{M}\,\hat{\rho}_{s}(n\delta t)\,\hat{M}^{\dagger}
=\displaystyle= ρ^s+ζδt[s1A^(A^ρ^s+ρ^sA^)+s2B^(B^ρ^s+ρ^sB^)s14(A^2ρ^s+ρ^sA^2)s24(B^2ρ^s+ρ^sB^2)]\displaystyle\hat{\rho}_{s}+\zeta\,\delta t\bigg{[}s_{1}\left\langle\hat{A}\right\rangle(\hat{A}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{A})+s_{2}\left\langle\hat{B}\right\rangle(\hat{B}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{B})-\frac{s_{1}}{4}(\hat{A}^{2}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{A}^{2})-\frac{s_{2}}{4}(\hat{B}^{2}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{B}^{2})\bigg{]}
+λ1ζ(A^ρ^s+ρ^sA^)dξ1+λ2ζ(B^ρ^s+ρ^sB^)dξ2+ζ2δt(λ12A^ρ^sA^+λ22B^ρ^sB^)+O(δt3/2).\displaystyle+\lambda_{1}\,\zeta\,(\hat{A}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{A})\,d\xi_{1}+\lambda_{2}\,\zeta\,(\hat{B}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{B})\,d\xi_{2}+\zeta^{2}\,\delta t\,(\lambda_{1}^{2}\,\hat{A}\,\hat{\rho}_{s}\,\hat{A}+\lambda_{2}^{2}\,\hat{B}\,\hat{\rho}_{s}\,\hat{B})+O\left(\delta t^{3/2}\right). (36)

The normalization constant for the state after the measurement reads

Tr(M^ρ^sM^)=\displaystyle\mathrm{Tr}\,(\hat{M}\,\hat{\rho}_{s}\,\hat{M}^{\dagger})= 1+2ζδt(s1A^2+s2B^2)\displaystyle 1+2\zeta\,\delta t\,\left(s_{1}\left\langle\hat{A}\right\rangle^{2}+s_{2}\left\langle\hat{B}\right\rangle^{2}\right)
+2λ1ζA^dξ1+2λ2ζB^dξ2+O(δt3/2).\displaystyle+2\lambda_{1}\,\zeta\,\left\langle\hat{A}\right\rangle\,d\xi_{1}+2\lambda_{2}\,\zeta\,\left\langle\hat{B}\right\rangle\,d\xi_{2}+O\left(\delta t^{3/2}\right). (37)

Applying (1+x)11x+x2(1+x)^{-1}\approx 1-x+x^{2} and keeping terms up to the first order of δt\delta t, we obtain the normalized state after the measurement,

ρ^s(nδt)=\displaystyle\hat{\rho}^{\prime}_{s}(n\delta t)= M^ρ^sM^Tr(M^ρ^sM^)\displaystyle\frac{\hat{M}\hat{\rho}_{s}\hat{M}^{\dagger}}{\mathrm{Tr}\,(\hat{M}\hat{\rho}_{s}\hat{M}^{\dagger})}
\displaystyle\approx ρ^ss1ζ4(A^2ρ^s+ρ^sA^22A^ρ^sA^)δts2ζ4(B^2ρ^s+ρ^sB^22B^ρ^sB^)δt+2s1ζ(A^ρ^s+ρ^sA^2A^ρ^s)dξ1\displaystyle\hat{\rho}_{s}-\frac{s_{1}\zeta}{4}(\hat{A}^{2}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{A}^{2}-2\hat{A}\hat{\rho}_{s}\hat{A})\,\delta t-\frac{s_{2}\zeta}{4}(\hat{B}^{2}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{B}^{2}-2\hat{B}\hat{\rho}_{s}\hat{B})\,\delta t+\sqrt{2s_{1}\zeta}\,\bigg{(}\frac{\hat{A}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{A}}{2}-\left\langle\hat{A}\right\rangle\hat{\rho}_{s}\bigg{)}\,d\xi_{1}
+2s2ζ(B^ρ^s+ρ^sB^2B^ρ^s)dξ2\displaystyle+\sqrt{2s_{2}\zeta}\,\bigg{(}\frac{\hat{B}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{B}}{2}-\left\langle\hat{B}\right\rangle\hat{\rho}_{s}\bigg{)}\,d\xi_{2}
=\displaystyle= ρ^sγ18[A^,[A^,ρ^s]]δtγ28[B^,[B^,ρ^s]]δt+γ1[(A^A^)ρ^s]dξ1+γ2[(B^B^)ρ^s]dξ2.\displaystyle\hat{\rho}_{s}-\frac{\gamma_{1}}{8}[\hat{A},[\hat{A},\hat{\rho}_{s}]]\,\delta t-\frac{\gamma_{2}}{8}[\hat{B},[\hat{B},\hat{\rho}_{s}]]\,\delta t+\sqrt{\gamma_{1}}\,\mathcal{H}\left[\left(\hat{A}-\left\langle\hat{A}\right\rangle\right)\,\hat{\rho}_{s}\right]\,d\xi_{1}+\sqrt{\gamma_{2}}\,\mathcal{H}\left[\left(\hat{B}-\left\langle\hat{B}\right\rangle\right)\,\hat{\rho}_{s}\right]\,d\xi_{2}. (38)

Here, the symbol [O^]\mathcal{H}[\hat{O}] is defined as the Hermitian part of operator O^\hat{O},

[O^]12(O^+O^).\displaystyle\mathcal{H}[\hat{O}]\equiv\frac{1}{2}(\hat{O}+\hat{O}^{\dagger}). (39)

Including the unitary evolution between the two consecutive measurements and taking the continuous limit, the conditioned master equation reads

dρ^s=\displaystyle d\hat{\rho}_{s}= i[H^s,ρ^s]dtγ18[A^,[A^,ρ^s]]dtγ28[B^,[B^,ρ^s]]dt\displaystyle-i[\hat{H}_{s},\hat{\rho}_{s}]\,dt-\frac{\gamma_{1}}{8}[\hat{A},[\hat{A},\hat{\rho}_{s}]]\,dt-\frac{\gamma_{2}}{8}[\hat{B},[\hat{B},\hat{\rho}_{s}]]\,dt
+γ1[(A^A^)ρ^s]dξ1\displaystyle+\sqrt{\gamma_{1}}\,\mathcal{H}\left[\left(\hat{A}-\left\langle\hat{A}\right\rangle\right)\hat{\rho}_{s}\right]\,d\xi_{1}
+γ2[(B^B^)ρ^s]dξ2.\displaystyle+\sqrt{\gamma_{2}}\,\mathcal{H}\left[\left(\hat{B}-\left\langle\hat{B}\right\rangle\right)\hat{\rho}_{s}\right]\,d\xi_{2}. (40)

III state preparation by the feedback control

We now propose a scheme to manipulate the state of a spin-1/21/2 system based on the generalized Arthurs-Kelly measurement model obtained in the previous section. For simultaneous and continuous measurement of the xx and yy components of the spin 𝑺^\bm{\hat{S}}, i.e., A^=σ^x/2\hat{A}=\hat{\sigma}_{x}/2 and B^=σ^y/2\hat{B}=\hat{\sigma}_{y}/2 with σ^x\hat{\sigma}_{x} and σ^y\hat{\sigma}_{y} being the Pauli matrices, the conditioned master equation (40) can be written as

dρ^s=\displaystyle d\hat{\rho}_{s}= i[H^s,ρ^s]dtΓx8[σ^x,[σ^x,ρ^s]]dtΓy8[σ^y,[σ^y,ρ^s]]dt\displaystyle-i[\hat{H}_{s},\hat{\rho}_{s}]dt-\frac{\Gamma_{x}}{8}[\hat{\sigma}_{x},[\hat{\sigma}_{x},\hat{\rho}_{s}]]dt-\frac{\Gamma_{y}}{8}[\hat{\sigma}_{y},[\hat{\sigma}_{y},\hat{\rho}_{s}]]dt
+Γx[(σ^xσ^x)ρ^s]dξx\displaystyle+\sqrt{\Gamma_{x}}\mathcal{H}\left[(\hat{\sigma}_{x}-\left\langle\hat{\sigma}_{x}\right\rangle)\,\hat{\rho}_{s}\right]\,d\xi_{x}
+Γy[(σ^yσ^y)ρ^s]dξy,\displaystyle+\sqrt{\Gamma_{y}}\mathcal{H}\left[(\hat{\sigma}_{y}-\left\langle\hat{\sigma}_{y}\right\rangle)\,\hat{\rho}_{s}\right]\,d\xi_{y}, (41)

where Γxγ1/4=s1ζ/2\Gamma_{x}\equiv\gamma_{1}/4=s_{1}\zeta/2 and Γyγ2/4=s2ζ/2\Gamma_{y}\equiv\gamma_{2}/4=s_{2}\zeta/2 are the measurement strengths of the xx and yy components of the spin, respectively. We assume that the system is in a static external magnetic field; as a consequence, the Hamiltonian of the system can be represented as

H^s=ωxσx^+ωyσ^y+ωzσ^z,\displaystyle\hat{H}_{s}=\omega_{x}\hat{\sigma_{x}}+\omega_{y}\hat{\sigma}_{y}+\omega_{z}\hat{\sigma}_{z}, (42)

where ωx\omega_{x}, ωy\omega_{y}, and ωz\omega_{z} can be set by the magnitude and the direction of the static external field.

The measurement signals σ¯x\bar{\sigma}_{x} and σ¯y\bar{\sigma}_{y} are defined as A. Levy

σ¯xdt\displaystyle\bar{\sigma}_{x}dt =σ^xdt+dξxΓx,\displaystyle=\left\langle\hat{\sigma}_{x}\right\rangle dt+\frac{d\xi_{x}}{\sqrt{\Gamma_{x}}}, (43)
σ¯ydt\displaystyle\bar{\sigma}_{y}dt =σ^ydt+dξyΓy,\displaystyle=\left\langle\hat{\sigma}_{y}\right\rangle dt+\frac{d\xi_{y}}{\sqrt{\Gamma_{y}}}, (44)

which will be fed back to the system without time delay T. L. Patti to control an additional external magnetic field 𝑩\bm{B} by the following feedback control Hamiltonian:

H^fdt=\displaystyle\hat{H}_{f}\,dt= 𝑩𝑺^dt\displaystyle\bm{B}\cdot\bm{\hat{S}}\,dt
=\displaystyle= (α1c¯+α1c¯)σ^xdt+(α2c¯+α2c¯)σ^ydt\displaystyle(\alpha_{1}\bar{c}+\alpha_{1}^{*}\bar{c}^{*})\hat{\sigma}_{x}\,dt+(\alpha_{2}\bar{c}+\alpha_{2}^{*}\bar{c}^{*})\hat{\sigma}_{y}\,dt
+(α3c¯+α3c¯)σ^zdt\displaystyle+(\alpha_{3}\bar{c}+\alpha_{3}^{*}\bar{c}^{*})\hat{\sigma}_{z}\,dt
=\displaystyle= c¯dt(α1σ^x+α2σ^y+α3σ^z)+H.c.,\displaystyle\bar{c}dt(\alpha_{1}\hat{\sigma}_{x}+\alpha_{2}\hat{\sigma}_{y}+\alpha_{3}\hat{\sigma}_{z})+\textrm{H.c.}, (45)

where αi\alpha_{i} (i=x,y,zi=x,y,z) is an arbitrary complex number used to control the ii component of the additional magnetic field 𝑩\bm{B}, c¯dt12(σ¯xiσ¯y)dt\bar{c}dt\equiv\frac{1}{2}(\bar{\sigma}_{x}-i\bar{\sigma}_{y})dt is the complex measurement signal, and H.c. is the Hermitian conjugate of the former term. Here, we have set the Lande factor and the Bohr magneton to be unity for simplicity. Equation (45) can be rewritten into an equivalent, but more compact form,

H^fdt=iκfc¯dtF^+H.c.,\displaystyle\hat{H}_{f}\,dt=-i\kappa_{f}\,\bar{c}\,dt\cdot\hat{F}+\textrm{H.c.}, (46)

where κf\kappa_{f} is an arbitrary real positive parameter called feedback control strength, and F^\hat{F} is a linear combination of σ^x\hat{\sigma}_{x}, σ^y\hat{\sigma}_{y}, and σ^z\hat{\sigma}_{z}, corresponding to F^=iκf1(α1σ^x+α2σ^y+α3σ^z)\hat{F}=i\kappa_{f}^{-1}(\alpha_{1}\hat{\sigma}_{x}+\alpha_{2}\hat{\sigma}_{y}+\alpha_{3}\hat{\sigma}_{z}) in terms of αi\alpha_{i} in Eq. (45).

Suppose the system is in the state ρ^s\hat{\rho}_{s} at time tt; the state of the system at t+dtt+dt after the simultaneous, continuous measurement and feedback control is given by exp(iH^fdt)(ρ^s+dρ^s)exp(iH^fdt)\exp(-i\hat{H}_{f}dt)\,(\hat{\rho}_{s}+d\hat{\rho}_{s})\,\exp(i\hat{H}_{f}dt). Within the first order in dtdt, we need to keep the following terms: ρ^s+dρ^s\hat{\rho}_{s}+d\hat{\rho}_{s}, i[H^fdt,ρ^s]-i[\hat{H}_{f}dt,\hat{\rho}_{s}], i[H^fdt,dρ^s]-i[\hat{H}_{f}dt,d\hat{\rho}_{s}], and 21[H^fdt,[H^fdt,ρ^s]]-2^{-1}[\hat{H}_{f}dt,[\hat{H}_{f}dt,\hat{\rho}_{s}]]. Note that the last one also has the first order of dtdt due to the Itô rule. By inserting Eqs. (43) and (44) into these terms, we obtain the ensemble-averaged master equation of the system under the simultaneous, continuous measurement and the feedback control,

dρ^sdt=\displaystyle\frac{d\hat{\rho}_{s}}{dt}= i[H^s,ρ^s]+Γy2𝒟[c^]ρ^s+Γy2𝒟[c^]ρ^s\displaystyle-i[\hat{H}_{s},\hat{\rho}_{s}]+\frac{\Gamma_{y}}{2}\mathcal{D}[\hat{c}]\hat{\rho}_{s}+\frac{\Gamma_{y}}{2}\mathcal{D}[\hat{c}^{\dagger}]\hat{\rho}_{s}
+ΓxΓy4𝒟[c^+c^]ρ^s+κf24Γx𝒟[i(F^F^)]ρ^s\displaystyle+\frac{\Gamma_{x}-\Gamma_{y}}{4}\mathcal{D}[\hat{c}+\hat{c}^{\dagger}]\hat{\rho}_{s}+\frac{\kappa_{f}^{2}}{4\Gamma_{x}}\mathcal{D}[i(\hat{F}-\hat{F}^{\dagger})]\hat{\rho}_{s}
+κf24Γy𝒟[F^+F^]ρ^sκf2([F^,c^ρ^s][F^,ρ^sc^]\displaystyle+\frac{\kappa_{f}^{2}}{4\Gamma_{y}}\mathcal{D}[\hat{F}+\hat{F}^{\dagger}]\hat{\rho}_{s}-\frac{\kappa_{f}}{2}\big{(}[\hat{F},\hat{c}\hat{\rho}_{s}]-[\hat{F}^{\dagger},\hat{\rho}_{s}\hat{c}^{\dagger}]
+[F^,ρ^sc^][F^,c^ρ^s]),\displaystyle+[\hat{F},\hat{\rho}_{s}\hat{c}]-[\hat{F}^{\dagger},\hat{c}^{\dagger}\hat{\rho}_{s}]\big{)}, (47)

where c^12(σ^xiσ^y)\hat{c}\equiv\frac{1}{2}(\hat{\sigma}_{x}-i\hat{\sigma}_{y}) is the lowering operator, and the superoperator 𝒟[O^]\mathcal{D}[\hat{O}] is defined for an arbitrary operator O^\hat{O} by

𝒟[O^]ρ^sO^ρ^sO^12(O^O^ρ^s+ρ^sO^O^).\displaystyle\mathcal{D}[\hat{O}]\,\hat{\rho}_{s}\equiv\hat{O}\hat{\rho}_{s}\hat{O}^{\dagger}-\frac{1}{2}\left(\hat{O}^{\dagger}\hat{O}\hat{\rho}_{s}+\hat{\rho}_{s}\hat{O}^{\dagger}\hat{O}\right). (48)

Equation (47) provides the general form of the evolution of the system. The form of the operator F^\hat{F} is to be chosen according to the target state. Note that, for F^=c^\hat{F}=\hat{c}^{\dagger} [i.e., α1=iκf/2\alpha_{1}=-i\kappa_{f}/2, α2=κf/2\alpha_{2}=\kappa_{f}/2, and α3=0\alpha_{3}=0 in Eq. (45)], Eq. (47) can be written in the Lindblad form,

dρ^sdt=i[H^s,ρ^s]+k1𝒟[c^]ρ^s+k2𝒟[c^]ρ^s+k3𝒟[c^+c^]ρ^s,\displaystyle\frac{d\hat{\rho}_{s}}{dt}=-i[\hat{H}_{s},\hat{\rho}_{s}]+k_{1}\mathcal{D}[\hat{c}]\hat{\rho}_{s}+k_{2}\mathcal{D}[\hat{c}^{\dagger}]\hat{\rho}_{s}+k_{3}\mathcal{D}[\hat{c}+\hat{c}^{\dagger}]\hat{\rho}_{s}, (49)

with

k1\displaystyle k_{1} Γy2+κf22Γx+κf,\displaystyle\equiv\frac{\Gamma_{y}}{2}+\frac{\kappa_{f}^{2}}{2\Gamma_{x}}+\kappa_{f}, (50)
k2\displaystyle k_{2} Γy2+κf22Γxκf,\displaystyle\equiv\frac{\Gamma_{y}}{2}+\frac{\kappa_{f}^{2}}{2\Gamma_{x}}-\kappa_{f}, (51)
k3\displaystyle k_{3} ΓxΓy4κf24Γx+κf24Γy.\displaystyle\equiv\frac{\Gamma_{x}-\Gamma_{y}}{4}-\frac{\kappa_{f}^{2}}{4\Gamma_{x}}+\frac{\kappa_{f}^{2}}{4\Gamma_{y}}. (52)

The first term in the right-hand side of Eq. (49) represents the unitary evolution governed by the static external field while the latter three terms represent the effect of the simultaneous measurement and the feedback control.

For the spin-1/21/2 system, it is more convenient to discuss the problem in the Bloch coordinate system and represent ρ^s\hat{\rho}_{s} with the basis σ^x\hat{\sigma}_{x}, σ^y\hat{\sigma}_{y}, σ^z\hat{\sigma}_{z}, and the unit operator I^\hat{I},

ρ^s=12(xσ^x+yσ^y+zσ^z+I^),\displaystyle\hat{\rho}_{s}=\frac{1}{2}(x\hat{\sigma}_{x}+y\hat{\sigma}_{y}+z\hat{\sigma}_{z}+\hat{I}), (53)

where (x,y,z)3(x,y,z)\in\mathbb{R}^{3} is the Bloch vector satisfying x2+y2+z21\sqrt{x^{2}+y^{2}+z^{2}}\leqslant 1. By inserting Eq. (53) into Eq. (49) and using Tr(σ^jρ^s)=j\mathrm{Tr}\,(\hat{\sigma}_{j}\hat{\rho}_{s})=j  (with j=x,y,zj=x,y,z), we obtain

x˙\displaystyle\dot{x} =2(ωyzωzy)k1+k22x,\displaystyle=2(\omega_{y}z-\omega_{z}y)-\frac{k_{1}+k_{2}}{2}x, (54)
y˙\displaystyle\dot{y} =2(ωzxωxz)k1+k2+4k32y,\displaystyle=2(\omega_{z}x-\omega_{x}z)-\frac{k_{1}+k_{2}+4k_{3}}{2}y, (55)
z˙\displaystyle\dot{z} =2(ωxyωyx)(k1+k2+2k3)z+k2k1.\displaystyle=2(\omega_{x}y-\omega_{y}x)-(k_{1}+k_{2}+2k_{3})z+k_{2}-k_{1}. (56)

The steady solution of these master equations is obtained by setting x˙=y˙=z˙=0\dot{x}=\dot{y}=\dot{z}=0 in Eqs. (54) – (56) note:explain ,

xs\displaystyle x_{s} =4η1(k2k1)[ωy(k1+k2+4k3)+4ωxωz],\displaystyle=4\eta^{-1}(k_{2}-k_{1})[\omega_{y}(k_{1}+k_{2}+4k_{3})+4\omega_{x}\omega_{z}], (57)
ys\displaystyle y_{s} =4η1(k1k2)[ωx(k1+k2)4ωyωz],\displaystyle=4\eta^{-1}(k_{1}-k_{2})[\omega_{x}(k_{1}+k_{2})-4\omega_{y}\omega_{z}], (58)
zs\displaystyle z_{s} =η1(k2k1)[(k1+k2)(k1+k2+4k3)+16ωz2],\displaystyle=\eta^{-1}(k_{2}-k_{1})\left[(k_{1}+k_{2})(k_{1}+k_{2}+4k_{3})+16\omega_{z}^{2}\right], (59)

with

η\displaystyle\eta\equiv (k1+k2)(k1+k2+2k3)(k1+k2+4k3)+8ωx2(k1+k2)\displaystyle(k_{1}+k_{2})(k_{1}+k_{2}+2k_{3})(k_{1}+k_{2}+4k_{3})+8\omega_{x}^{2}(k_{1}+k_{2})
+8ωy2(k1+k2+4k3)+16ωz2(k1+k2+2k3).\displaystyle+8\omega_{y}^{2}(k_{1}+k_{2}+4k_{3})+16\omega_{z}^{2}(k_{1}+k_{2}+2k_{3}). (60)

Equations (57) – (60) provide a guideline to realize the steady state of the system by the static external field, the simultaneous and continuous measurement, and the feedback control. One of the most important cases is the one in which the direction of the external magnetic field is along the zz axis, where the Hamiltonian of the system H^s\hat{H}_{s} is diagonal with ωx=ωy=0\omega_{x}=\omega_{y}=0 and ωz0\omega_{z}\neq 0. Then the steady state given by Eqs. (57) – (59) becomes

xs\displaystyle x_{s} =0,\displaystyle=0, (61)
ys\displaystyle y_{s} =0,\displaystyle=0, (62)
zs\displaystyle z_{s} =k2k1k1+k2+2k3,\displaystyle=\frac{k_{2}-k_{1}}{k_{1}+k_{2}+2k_{3}}, (63)

which is diagonal in the energy basis so that it can be identified as a thermal state with some effective temperature. This means that the simultaneous measurement and feedback control introduced above effectively serve as a heat bath A. Levy . When we perform both the measurement and the feedback control on the system for a sufficiently long time, the system eventually reaches a thermal state. Since zsz_{s} is independent of the sign of ωz\omega_{z} as seen in Eqs. (59) and (60), we can assume ωz>0\omega_{z}>0 without loss of generality, and the effective temperature TeffT_{\rm{eff}} can be obtained as

Teff=2ωzkB(lnk1+k3k2+k3)1,\displaystyle T_{\rm{eff}}=\frac{2\omega_{z}}{k_{B}}\left(\ln\frac{k_{1}+k_{3}}{k_{2}+k_{3}}\right)^{-1}, (64)

where kBk_{B} is the Boltzmann constant. Since (k1+k3)/(k2+k3)(k_{1}+k_{3})/(k_{2}+k_{3}) is always larger than 1, the effective temperature TeffT_{\rm{eff}} is a monotonically increasing function of ωz\omega_{z}, and TeffT_{\rm{eff}} satisfies 0Teff<0\leqslant T_{\rm{eff}}<\infty. Thus, we can prepare the system in a diagonal steady state with an arbitrary positive effective temperature by setting proper k1k_{1}, k2k_{2}, k3k_{3}, and ωz\omega_{z} under ωx=ωy=0\omega_{x}=\omega_{y}=0. In order to see the dependence of TeffT_{\rm{eff}} on parameters Γx\Gamma_{x}, Γy\Gamma_{y}, and κf\kappa_{f}, we substitute Eqs. (50) – (52) into Eq. (63) and obtain

zs=4(Γxκf+κfΓx+Γyκf+κfΓy)1.\displaystyle z_{s}=-4\left(\frac{\Gamma_{x}}{\kappa_{f}}+\frac{\kappa_{f}}{\Gamma_{x}}+\frac{\Gamma_{y}}{\kappa_{f}}+\frac{\kappa_{f}}{\Gamma_{y}}\right)^{-1}. (65)

Here, zsz_{s} first decreases when Γx/κf\Gamma_{x}/\kappa_{f} and Γy/κf\Gamma_{y}/\kappa_{f} increase from 0 to 11, and then increases when Γx/κf\Gamma_{x}/\kappa_{f} and Γy/κf\Gamma_{y}/\kappa_{f} increase from 11 to infinity. zsz_{s} takes the minimum at Γx/κf=Γy/κf=1\Gamma_{x}/\kappa_{f}=\Gamma_{y}/\kappa_{f}=1. According to Eq. (53), the probabilities in the excited state and the ground state are proportional to (1+zs)(1+z_{s}) and (1zs)(1-z_{s}), respectively. When zsz_{s} decreases, the probability of the system in the excited state becomes smaller, which means that the effective temperature TeffT_{\rm{eff}} is lower. Therefore, TeffT_{\rm{eff}} first decreases and then increases when Γx/κf\Gamma_{x}/\kappa_{f} and Γy/κf\Gamma_{y}/\kappa_{f} increase from 0 to infinity, and TeffT_{\rm{eff}} takes the minimum value of zero at Γx/κf=Γy/κf=1\Gamma_{x}/\kappa_{f}=\Gamma_{y}/\kappa_{f}=1. Figure 2 shows the contours of TeffT_{\rm{eff}} with respect to Γx\Gamma_{x} and Γy\Gamma_{y} for ωx=ωy=0\omega_{x}=\omega_{y}=0.

Refer to caption
Figure 2: Contours of effective temperature TeffT_{\rm{eff}} with respect to Γx\Gamma_{x} and Γy\Gamma_{y} for ωx=ωy=0\omega_{x}=\omega_{y}=0. Here, we have set κf\kappa_{f} = ωz\omega_{z} = kBk_{B} = 1 for simplicity. TeffT_{\rm eff} takes the minimum, Teff=0T_{\rm{eff}}=0, at Γx=Γy=1\Gamma_{x}=\Gamma_{y}=1.

Besides the final effective temperature, the timescale for relaxation to the asymptotic steady state is another important quantity. We first consider z(t)z(t), which can be easily obtained from Eq. (56) with ωx=ωy=0\omega_{x}=\omega_{y}=0:

z(t)=k2k1k1+k2+2k3+C1e(k1+k2+2k3)t,\displaystyle z(t)=\frac{k_{2}-k_{1}}{k_{1}+k_{2}+2k_{3}}+C_{1}e^{-(k_{1}+k_{2}+2k_{3})t}, (66)

where C1C_{1} is a constant determined by the initial condition z(t=0)z(t=0). From Eq. (66), the relaxation time τz\tau_{z} of the spin-zz component can be defined as

τz\displaystyle\tau_{z}\equiv (k1+k2+2k3)1\displaystyle(k_{1}+k_{2}+2k_{3})^{-1}
=\displaystyle= 2(Γx+Γy+κf2Γx+κf2Γy)1.\displaystyle 2\left(\Gamma_{x}+\Gamma_{y}+\frac{\kappa_{f}^{2}}{\Gamma_{x}}+\frac{\kappa_{f}^{2}}{\Gamma_{y}}\right)^{-1}. (67)

When Γi1\Gamma_{i}\gg 1 or Γiκf2\Gamma_{i}\ll\kappa_{f}^{2} (with i=xi=x or yy), the relaxation time τz\tau_{z} is very short, which means the system can reach the steady state very quickly.

Next, we discuss x(t)x(t) and y(t)y(t). Equations (54) and (55) with ωx=ωy=0\omega_{x}=\omega_{y}=0 can be written as

x¨\displaystyle\ddot{x} =(k1+k2+2k3)x˙η4(k1+k2+2k3)x,\displaystyle=-(k_{1}+k_{2}+2k_{3})\dot{x}-\frac{\eta}{4(k_{1}+k_{2}+2k_{3})}x, (68)
y\displaystyle y =12ωz(x˙+k1+k22x).\displaystyle=-\frac{1}{2\omega_{z}}\left(\dot{x}+\frac{k_{1}+k_{2}}{2}x\right). (69)

The corresponding characteristic equation for Eq. (68) is

μ2(k1+k2+2k3)μ+η4(k1+k2+2k3)=0,\displaystyle\mu^{2}-(k_{1}+k_{2}+2k_{3})\mu+\frac{\eta}{4(k_{1}+k_{2}+2k_{3})}=0, (70)

and the solution of Eq. (70) is:

μ±=12[(k1+k2+2k3)±Δ]\displaystyle\mu_{\pm}=\frac{1}{2}\left[(k_{1}+k_{2}+2k_{3})\pm\sqrt{\Delta}\right] (71)

with

Δ\displaystyle\Delta (k1+k2+2k3)2ηk1+k2+2k3\displaystyle\equiv(k_{1}+k_{2}+2k_{3})^{2}-\frac{\eta}{k_{1}+k_{2}+2k_{3}}
=4k3216ωz2.\displaystyle=4k_{3}^{2}-16\omega_{z}^{2}. (72)

The solutions of Eqs. (68) and (69) are:

x(t)=\displaystyle x(t)= (C2+C3t)ek1+k2+2k32t,\displaystyle(C_{2}+C_{3}t)e^{-\frac{k_{1}+k_{2}+2k_{3}}{2}t}, (73)
y(t)=\displaystyle y(t)= 12ωz[k3C2+(1k3t)C3]ek1+k2+2k32t\displaystyle-\frac{1}{2\omega_{z}}\left[-k_{3}C_{2}+\left(1-k_{3}t\right)C_{3}\right]e^{-\frac{k_{1}+k_{2}+2k_{3}}{2}t} (74)

for Δ=0\Delta=0, and

x(t)=\displaystyle x(t)= C2eμ+t+C3eμt,\displaystyle C_{2}^{\prime}e^{-\mu_{+}t}+C_{3}^{\prime}e^{-\mu_{-}t}, (75)
y(t)=\displaystyle y(t)= 12ωz[C2(k1+k22μ+)eμ+t\displaystyle-\frac{1}{2\omega_{z}}\left[C_{2}^{\prime}\left(\frac{k_{1}+k_{2}}{2}-\mu_{+}\right)e^{-\mu_{+}t}\right.
+C3(k1+k22μ)eμt]\displaystyle\left.+C_{3}^{\prime}\left(\frac{k_{1}+k_{2}}{2}-\mu_{-}\right)e^{-\mu_{-}t}\right] (76)

for Δ0\Delta\neq 0, where C2C_{2}, C3C_{3}, C2C_{2}^{\prime}, and C3C_{3}^{\prime} are constants determined by the initial condition x(t=0)x(t=0) and y(t=0)y(t=0). When Δ0\Delta\leqslant 0, both x(t)x(t) and y(t)y(t) decay as exp(k1+k2+2k32t)\exp{\left(-\frac{k_{1}+k_{2}+2k_{3}}{2}t\right)}. Thus, the relaxation time τx\tau_{x} and τy\tau_{y} of the xx and yy components of the spin can be defined as

τx=τy\displaystyle\tau_{x}=\tau_{y}\equiv 2(k1+k2+2k3)1\displaystyle 2(k_{1}+k_{2}+2k_{3})^{-1}
=\displaystyle= 2τz.\displaystyle 2\tau_{z}. (77)

According to the previous discussion, the system reaches the steady state very quickly if Γi1\Gamma_{i}\gg 1 or Γiκf2\Gamma_{i}\ll\kappa_{f}^{2}. When Δ>0\Delta>0, the decay rates of x(t)x(t) and y(t)y(t) are mainly determined by the term with exp(μt)\exp{(-\mu_{-}t)} since μ<μ+\mu_{-}<\mu_{+}. Consequently, the definition of the relaxation time τx\tau_{x} and τy\tau_{y} is

τx=τy\displaystyle\tau_{x}=\tau_{y}\equiv μ1\displaystyle\mu_{-}^{-1}
=\displaystyle= 2(k1+k2+2k3Δ)1\displaystyle 2\left(k_{1}+k_{2}+2k_{3}-\sqrt{\Delta}\right)^{-1}
\displaystyle\leqslant 2(k1+k2+2k34k32)1\displaystyle 2\left(k_{1}+k_{2}+2k_{3}-\sqrt{4k_{3}^{2}}\right)^{-1}
=\displaystyle= 2(k1+k2+2k32|k3|)1.\displaystyle 2\left(k_{1}+k_{2}+2k_{3}-2\left|k_{3}\right|\right)^{-1}. (78)

When k30k_{3}\geqslant 0, Eq. (78) reads

τx=τy\displaystyle\tau_{x}=\tau_{y}\leqslant 2(k1+k2)1\displaystyle 2(k_{1}+k_{2})^{-1}
=\displaystyle= 2(Γy+κf2Γx)1.\displaystyle 2\left(\Gamma_{y}+\frac{\kappa_{f}^{2}}{\Gamma_{x}}\right)^{-1}. (79)

The relaxation time is very short if Γy1\Gamma_{y}\gg 1 or Γxκf2\Gamma_{x}\ll\kappa_{f}^{2}. When k3<0k_{3}<0 on the other hand, Eq. (78) reads

τx=τy\displaystyle\tau_{x}=\tau_{y}\leqslant 2(k1+k2+4k3)1\displaystyle 2(k_{1}+k_{2}+4k_{3})^{-1}
=\displaystyle= 2(Γx+κf2Γy)1,\displaystyle 2\left(\Gamma_{x}+\frac{\kappa_{f}^{2}}{\Gamma_{y}}\right)^{-1}, (80)

and the relaxation time is very short if Γx1\Gamma_{x}\gg 1 or Γyκf2\Gamma_{y}\ll\kappa_{f}^{2}. In summary, the relaxation time of the system is controllable by the strengths of the measurement and the feedback control, and the system can reach the steady state very quickly if Γx,Γy1\Gamma_{x},\Gamma_{y}\gg 1 or Γx,Γyκf2\Gamma_{x},\Gamma_{y}\ll\kappa_{f}^{2}.

Refer to caption
Figure 3: Contours of xsx_{s} with respect to Γx\Gamma_{x} and Γy\Gamma_{y} at (a) (ωx,ωy)=(0.1,0.1)(\omega_{x},\omega_{y})=(0.1,0.1), (b) (ωx,ωy)=(0.5,0.1)(\omega_{x},\omega_{y})=(0.5,0.1), and (c) (ωx,ωy)=(0.1,0.5)(\omega_{x},\omega_{y})=(0.1,0.5). Here we set ωz=0\omega_{z}=0 and κf=1\kappa_{f}=1.

Let us now discuss more general cases where the direction of the static external magnetic field is arbitrary, i.e., ωx\omega_{x}, ωy\omega_{y}, and ωz\omega_{z} are nonzero in general. In such cases, the Hamiltonian H^s\hat{H}_{s} contains off-diagonal terms and these off-diagonal terms generate coherence between the ground state and the excited state of the operator σ^z\hat{\sigma}_{z}, which leads to the situation in which the steady state is no longer a thermal state. To get a better understanding of the effect of the off-diagonal terms, we set ωz=0\omega_{z}=0 and keep ωx\omega_{x} and ωy\omega_{y} to be nonzero. Then xsx_{s} and ysy_{s}, which characterize the effects of the off-diagonal terms on the steady state become

xs\displaystyle x_{s} =4η1ωy(k2k1)(k1+k2+4k3),\displaystyle=4\eta^{-1}\omega_{y}(k_{2}-k_{1})(k_{1}+k_{2}+4k_{3}), (81)
ys\displaystyle y_{s} =4η1ωx(k1k2)(k1+k2).\displaystyle=4\eta^{-1}\omega_{x}(k_{1}-k_{2})(k_{1}+k_{2}). (82)

From Eqs. (81) and (82), we can clearly see that xsx_{s} is more sensitive to ωy\omega_{y} than ωx\omega_{x} while ysy_{s} is more sensitive to ωx\omega_{x} than ωy\omega_{y}. Let us focus on xsx_{s} as an example. Figure 3 shows xsx_{s} as a function of Γx\Gamma_{x} and Γy\Gamma_{y} for different values of (ωx,ωy)(\omega_{x},\omega_{y}): (0.1,0.1)(0.1,0.1) [Fig. 3(a)], (0.5,0.1)(0.5,0.1) [Fig. 3(b)], and (0.1,0.5)(0.1,0.5) [Fig. 3(c)]. One can clearly see that by comparing Figs. 3(a) and 3(b), the contours change only a little by changing ωx\omega_{x} with ωy\omega_{y} fixed, while by comparing Figs. 3(a) and 3(c), the contours drastically change by changing ωy\omega_{y} with ωx\omega_{x} fixed. Therefore, to control xsx_{s} over a wide range, we should tune ωy\omega_{y} instead of ωx\omega_{x}; on the other hand, to control xsx_{s} accurately, we should first choose an appropriate value of ωy\omega_{y} and then tune ωx\omega_{x} with ωy\omega_{y} fixed.

Refer to caption
Figure 4: Boundaries of the region of possible (xs,ys)(x_{s},y_{s}) for different values of (ωx,ωy)(\omega_{x},\omega_{y}). Values of (xs,ys)(x_{s},y_{s}) below the dashed line are realizable for each (ωx,ωy)(\omega_{x},\omega_{y}). (a) ωx=0.5\omega_{x}=0.5 and ωy=0.1\omega_{y}=-0.1 (blue dashed line), 0.5-0.5 (red dashed line), and 1-1 (green dashed line). (b) ωy=0.5\omega_{y}=-0.5 and ωx=0.1\omega_{x}=0.1 (blue dashed line), 0.50.5 (red dashed line), and 11 (green dashed line). Here, we set κf=1\kappa_{f}=1, and negative values of ωy\omega_{y} to get positive xsx_{s}.

Figure 3 also implies that the range of the accessible values of xsx_{s} and ysy_{s} by varying Γx\Gamma_{x} and Γy\Gamma_{y} depends on ωx\omega_{x} and ωy\omega_{y}. To get a better understanding of this dependence, we show the region of possible values of (xs,ys)(x_{s},y_{s}) for several different values of (ωx,ωy)(\omega_{x},\omega_{y}) in Fig. 4. Figure 4(a) shows the boundaries of this region for different values of ωy=0.1\omega_{y}=-0.1, 0.5-0.5, and 1-1, with ωx\omega_{x} fixed at 0.50.5. Note that these boundaries are straight lines within the numerical accuracy. With increasing the absolute value of ωy\omega_{y} from zero, the range of the possible values of xsx_{s} first increases and becomes maximum at |ωy|=0.5|\omega_{y}|=0.5, then decreases, while the range of the possible values of ysy_{s} is unchanged from 0ys10\leqslant y_{s}\leqslant 1. On the other hand, Fig. 4(b) shows the boundaries for different values of ωx=0.1\omega_{x}=0.1, 0.50.5, and 11, with ωy\omega_{y} fixed at 0.5-0.5. The result is similar to that of Fig. 4(a), but xsx_{s} and ysy_{s} are switched: As ωx\omega_{x} increases from zero, the range of the possible values of ysy_{s} first increases and becomes maximum at ωx=0.5\omega_{x}=0.5, then decreases, while the range of the possible values of xsx_{s} is unchanged from 0xs10\leqslant x_{s}\leqslant 1. These results are consistent with the discussion in the last paragraph, and they also highlight the importance of choosing parameters ωx\omega_{x} and ωy\omega_{y} properly in preparing the state of the system. A given target steady state with some xsx_{s} and ysy_{s} is realizable only for parameters (ωx,ωy)(\omega_{x},\omega_{y}) in some region.

IV Conclusion

In summary, we have generalized the Arthurs-Kelly measurement model for a single-shot, simultaneous measurement to two arbitrary observables of the system whose commutator is not necessarily a cc-number. We have found that this generalized measurement model is valid only when the coupling between the system and the detectors is sufficiently weak. By applying this generalized model to the continuous measurement of two arbitrary observables, we have derived both unconditioned and conditioned master equations. We have shown that the unconditioned master equation takes the Lindblad form in the continuous limit, even if the coupling is not infinitesimally small. Moreover, we have found that there is no effect of the interplay of the two measurements in the continuous limit, even if the two observables are noncommutative and their commutator is not a cc-number. Finally, taking a spin-1/21/2 system as an example, we have illustrated that we can prepare a designated state as an asymptotic steady state of the time evolution by a static external field, the simultaneous, continuous measurement, and the feedback control based on the formalism derived in this work. We have obtained analytical expressions of the steady state and the timescale of the relaxation to the steady state, which offer a guiding principle for controlling the system. We have demonstrated that by appropriately setting the static external field and the strengths of the measurement and the feedback, we can control both the populations of the ground and the excited states and the coherence between them. Our results show that feedback control based on simultaneous, continuous measurement of multiple observables is one of the promising techniques which allows us to control the quantum state in a versatile manner.

Acknowledgements.
We thank Luis Pedro García-Pintos and Peter Talkner for helpful discussions and comments. This work was supported by NSF of China (Grants No. 11975199 and No. 11674283), the Zhejiang Provincial Natural Science Foundation Key Project (Grant No. LZ 19A050001), the Fundamental Research Funds for the Central Universities (Grants No. 2017QNA3005 and No. 2018QNA3004), and by the Zhejiang University 100 Plan.

References