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Ramsey Interferometry as Quantum Estimation

Ramsey interferometry estimates a parameter by preparing coherence, allowing a relative phase to accumulate, and converting that phase into a measured population. Its physical sequence is often summarized as

prepare⟶encode ϕ⟶choose analysis phase⟶measure.\text{prepare} \longrightarrow \text{encode }\phi \longrightarrow \text{choose analysis phase} \longrightarrow \text{measure}.

The population fringe is only the visible part of the protocol. A complete sensing statement must also specify the likelihood, working point, prior or capture range, interrogation and dead times, coherence loss, readout errors, estimator, uncertainty calibration, and comparison resource. Ramsey interferometry is therefore both a coherent-control primitive and a compact laboratory for quantum estimation theory.

Required background. Parameter estimation, Fisher information, and Cramér–Rao bounds supply the likelihood and local precision bounds; the standard quantum limit gives the independent-probe reference. Projective measurement explains the binary readout.

The AMO treatment of Ramsey interferometry derives the pulse dynamics and finite-pulse line shape. Here the focus is the information in the outcomes, frequency ambiguity, and the choice of interrogation time.

Consider a two-level probe with basis states ∣0⟩|0\rangle and ∣1⟩|1\rangle. An ideal preparation pulse creates an equatorial state, which may be written

∣+x⟩=∣0⟩+∣1⟩2.|+x\rangle = \frac{|0\rangle+|1\rangle}{\sqrt2}.

During the sensing interval, the unknown parameter produces a relative phase ϕ\phi. At the end of the interval the state is

∣ψϕ⟩=∣0⟩+eiϕ∣1⟩2.|\psi_\phi\rangle = \frac{ |0\rangle+e^{i\phi}|1\rangle }{\sqrt2}.

An analysis pulse with controllable phase θ\theta selects an equatorial measurement axis. With a convenient convention, the probability of the outcome x=1x=1 is

pθ(1∣ϕ)=12[1+sin⁡(ϕ−θ)].p_\theta(1|\phi) = \frac12 \left[ 1+\sin(\phi-\theta) \right].

For example, on the encoded qubit this outcome corresponds to the effect

Eθ,1=I−sin⁡θ σx+cos⁡θ σy2,pθ(1∣ϕ)=Tr⁡(ρϕEθ,1).E_{\theta,1}=\frac{I-\sin\theta\,\sigma_x+\cos\theta\,\sigma_y}{2}, \qquad p_\theta(1|\phi)=\operatorname{Tr}(\rho_\phi E_{\theta,1}).

Changing pulse conventions can replace the sine by a cosine or reverse its sign. Nothing operational changes if the same convention is used for the state, analysis phase, and estimator. The parameter θ\theta is not cosmetic: it moves the high-slope region of the fringe to the current estimate of ϕ\phi.

Loss of coherence reduces the fringe contrast. A common effective model is

pθ(1∣ϕ,C)=12[1+Csin⁡(ϕ−θ)],0≤C≤1.\begin{aligned} p_\theta(1|\phi,C) &= \frac12 \left[ 1+C\sin(\phi-\theta) \right], \\ 0&\le C\le 1. \end{aligned}

Here CC can include dephasing, inhomogeneous broadening, imperfect preparation, and analysis-pulse errors. Those mechanisms should be separated when the scientific claim depends on their interpretation, even if they enter the simplest likelihood through the same observed contrast.

A single projective readout does not reveal a probability or a phase. It produces one bit. For NN independent probes exposed to the same phase in one shot, let KK be the number of outcomes equal to one. Conditional on fixed ϕ\phi, CC, and θ\theta,

K∼Binomial⁡(N,pθ(1∣ϕ,C)).K \sim \operatorname{Binomial} \left( N,p_\theta(1|\phi,C) \right).

For settings indexed by jj, the likelihood is

L(ϕ,C)=∏j(NjKj)pjKj(1−pj)Nj−Kj,\mathcal L(\phi,C) = \prod_j {N_j\choose K_j} p_j^{K_j} (1-p_j)^{N_j-K_j},

with

pj=pθj(1∣ϕj,Cj).p_j = p_{\theta_j}(1|\phi_j,C_j).

The index can represent repeated shots, different analysis phases, different interrogation times, or controlled calibration settings. Writing this likelihood before choosing an estimator exposes several issues that a fringe plot can hide:

  • ϕ\phi is periodic and may not be globally identifiable;
  • contrast and offset can be nuisance parameters;
  • outcomes within a shot may cease to be independent under common-mode noise;
  • postselection changes the likelihood and accepted resource count;
  • drift can make nominally repeated trials non-identical.

The sufficient statistic is KK only under the independent, identical Bernoulli model. Time tags, detector channels, or individual-probe labels can carry additional information when noise or readout varies across the data.

Suppose the controller keeps the interferometer near ϕ=θ\phi=\theta, where the sine fringe crosses one half. If f=K/Nf=K/N is the measured excitation fraction, a local linear estimator is

ϕ^≃θ+2f−1C.\widehat\phi \simeq \theta + \frac{2f-1}{C}.

At the working point, p=1/2p=1/2 and

Var⁡(f)=14N.\operatorname{Var}(f) = \frac{1}{4N}.

Error propagation therefore gives

Var⁡(ϕ^)≃1NC2.\operatorname{Var}(\widehat\phi) \simeq \frac{1}{NC^2}.

For ν\nu statistically independent shots with stable settings,

Var⁡(ϕ^)≃1νNC2.\operatorname{Var}(\widehat\phi) \simeq \frac{1}{\nu NC^2}.

At C=1C=1, this is the independent-probe standard quantum limit for phase. The word projection describes the Bernoulli population fluctuations of a coherent superposition; it does not mean that every measured variance is quantum projection noise. Atom-number fluctuations, detector noise, phase jitter, and technical state-preparation noise must be modeled or bounded separately.

The estimator above is locally unbiased exactly at the calibrated working point: its mean equals ϕ\phi there and has derivative one. Away from that point its mean is θ+sin⁡(ϕ−θ)\theta+\sin(\phi-\theta), so fringe curvature creates bias; for sufficiently low CC, it can also return values outside the chosen phase branch. A maximum-likelihood or Bayesian estimator using the full periodic likelihood is usually preferable when the phase uncertainty is not already small.

For one binary outcome, the classical Fisher information for ϕ\phi is

F1(ϕ;θ,C)=(∂ϕpθ)2pθ(1−pθ).F_1(\phi;\theta,C) = \frac{ \left(\partial_\phi p_\theta\right)^2 }{ p_\theta(1-p_\theta) }.

Substituting the contrast-reduced sine fringe gives

F1=C2cos⁡2(ϕ−θ)1−C2sin⁡2(ϕ−θ).F_1 = \frac{ C^2\cos^2(\phi-\theta) }{ 1-C^2\sin^2(\phi-\theta) }.

At the quadrature working point,

F1(θ;θ,C)=C2.F_1(\theta;\theta,C) = C^2.

Independent probes and shots add information:

Ftot=νNC2F_{\mathrm{tot}} = \nu N C^2

at that point. The local Cramér–Rao bound then reproduces the projection-noise result,

Var⁡(ϕ^)≥1νNC2.\operatorname{Var}(\widehat\phi) \ge \frac{1}{\nu NC^2}.

For imperfect contrast, the fringe extrema contain little local information because their slopes vanish. In the mathematical C=1C=1 model the expression has a limiting value away from the extrema, but an exactly deterministic outcome is a nonregular operating point and is not robust to model error. Precision experiments deliberately use a high-slope discriminator rather than relying on that singular limit.

If CC describes the encoded state before measurement and is independent of the unknown phase, an equatorial qubit with dephasing can be written

ρϕ=12[I+C(cos⁡ϕ σx+sin⁡ϕ σy)].\rho_\phi = \frac12 \left[ I + C\left( \cos\phi\,\sigma_x + \sin\phi\,\sigma_y \right) \right].

Its quantum Fisher information for ϕ\phi is

FQ[ρϕ]=C2.F_Q[\rho_\phi] = C^2.

The quadrature Ramsey measurement attains this value locally. This example is important because it shows what measurement optimization means in practice: the QFI is not merely an abstract bound; an analysis phase aligned to the current estimate implements an optimal local measurement for this model.

Three qualifications remain:

  1. the optimal axis depends on the unknown phase, so a prior, pilot estimate, or adaptive controller is needed;
  2. QFI is local and does not resolve the periodic phase aliases;
  3. an achieved detector likelihood may contain SPAM errors or nuisance parameters absent from the state-only model.

The general distinctions between implemented Fisher information, SLD QFI, and attainable multiparameter bounds belong to Classical and Quantum Fisher Information.

For a constant detuning δω\delta\omega accumulated over free-evolution time TT,

ϕ=δωT.\phi = \delta\omega T.

Parameter transformation gives

Fδω=T2Fϕ.F_{\delta\omega} = T^2F_\phi.

Thus one independent probe at the optimal working point carries

Fδω=C(T)2T2.F_{\delta\omega} = C(T)^2T^2.

For a signal parameter λ\lambda coupled through an instantaneous angular frequency shift Ω(λ,t)\Omega(\lambda,t), ideal Ramsey evolution gives

ϕ(λ)=∫0TΩ(λ,t) dt.\phi(\lambda) = \int_0^T \Omega(\lambda,t) \,dt.

More generally, control modulation introduces a sensitivity function y(t)y(t):

ϕ(λ)=∫0Ty(t)Ω(λ,t) dt.\phi(\lambda) = \int_0^T y(t)\Omega(\lambda,t) \,dt.

For ordinary free precession, y(t)=1y(t)=1 between the two pulses. If the contrast is independent of λ\lambda and readout is at quadrature, the parameter information is

Fλ=C2(∂ϕ∂λ)2.F_\lambda = C^2 \left( \frac{\partial\phi}{\partial\lambda} \right)^2.

This formula separates three design ingredients: coherent response, contrast, and readout. It also makes units explicit. A phase sensitivity, a frequency sensitivity, and a magnetic-field sensitivity are not interchangeable without the response coefficient and interrogation time.

Longer free evolution increases phase response, but a real experiment pays for state preparation, control, measurement, and reset. Let

Tc=T+tdT_c = T+t_{\mathrm d}

be the cycle time, where tdt_{\mathrm d} collects dead time and overhead. For a large number of cycles in total averaging time τ\tau, the number of independent cycles is approximately ν=τ/Tc\nu=\tau/T_c. For NN independent probes per cycle,

Var⁡(δω^)≥TcτNC(T)2T2.\operatorname{Var}(\widehat{\delta\omega}) \ge \frac{T_c}{ \tau N C(T)^2T^2 }.

The frequency information rate is therefore

F˙δω=NC(T)2T2Tc.\dot F_{\delta\omega} = \frac{NC(T)^2T^2}{T_c}.

For a constant response ∂λϕ=κT\partial_\lambda\phi=\kappa T, a convenient sensitivity coefficient is

ηλ≡τ Δλ^≥Tc∣κ∣C(T)TN.\eta_\lambda \equiv \sqrt{\tau} \,\Delta\widehat\lambda \ge \frac{ \sqrt{T_c} }{ |\kappa| C(T)T\sqrt N }.

This is why the smallest one-shot phase variance need not identify the best sensor. A protocol can improve one shot while losing through slower cycles, lower duty factor, or reduced accepted-shot probability.

For a stretched-exponential Ramsey contrast

C(T)=exp⁡[−(T/T2∗)q],C(T) = \exp\left[-(T/T_2^*)^q\right],

with q>0q>0 and negligible dead time, maximizing information per unit time gives

Topt=T2∗(12q)1/q.T_{\mathrm{opt}} = T_2^* \left( \frac{1}{2q} \right)^{1/q}.

With nonzero dead time, the optimum solves

2T−1T+td−2qTq−1(T2∗)q=0.\frac{2}{T} - \frac{1}{T+t_{\mathrm d}} - \frac{2qT^{q-1}}{(T_2^*)^q} = 0.

The optimal TT depends on the objective. Maximizing single-shot frequency information, information per wall-clock time, bandwidth, or tracking performance produces different answers.

A Ramsey fringe is periodic:

pθ(1∣ϕ+2πm,C)=pθ(1∣ϕ,C),m∈Z.p_\theta(1|\phi+2\pi m,C) = p_\theta(1|\phi,C), \qquad m\in\mathbb Z.

For fixed TT, frequency values separated by 2π/T2\pi/T are aliases. A local uncertainty such as 1/(CTNν)1/(CT\sqrt{N\nu}) is meaningful only after the correct fringe branch has been identified. If the prior support is broader than one period, a single interrogation time cannot determine the frequency globally.

Two analysis phases can distinguish the reflection ambiguity of one sine fringe. For settings θ\theta and θ+π/2\theta+\pi/2, define, with known C>0C>0,

s^=2fθ−1C,c^=−2fθ+π/2−1C.\widehat s=\frac{2f_\theta-1}{C},\qquad \widehat c=-\frac{2f_{\theta+\pi/2}-1}{C}.

The minus sign follows from the sine convention: sin⁡(ϕ−θ−π/2)=−cos⁡(ϕ−θ)\sin(\phi-\theta-\pi/2)=-\cos(\phi-\theta). The circular phase estimate is

ϕ^=θ+atan2⁡(s^,c^).\widehat\phi = \theta + \operatorname{atan2} \left( \widehat s, \widehat c \right).

Quadrature readout distinguishes phase within a 2π2\pi interval but does not remove the integer alias. Low contrast also makes the angle estimator non-Gaussian; near the origin of the estimated quadrature plane, a symmetric confidence region is usually misleading.

Dynamic range is not just the fringe period. It also depends on prior knowledge, control range, sampling schedule, update latency, drift between settings, and the allowed probability of a cycle slip. A sensitivity number without an unambiguous range or tracking model is incomplete when the signal is not already locked near quadrature.

Broad-range protocols combine short and long interrogation times. A short time has weak phase leverage but a wide frequency period; a long time has high local resolution but many aliases. A geometric schedule such as

Tk=2kT0T_k = 2^kT_0

can identify coarse frequency bits before refining the estimate. Repetitions at each scale suppress branch errors.

For a fixed unknown angular detuning λ\lambda, each duration encodes ϕj=λTj\phi_j=\lambda T_j. In a Bayesian implementation, the posterior after outcome xjx_j is

πj(λ)∝p(xj∣λTj,θj)πj−1(λ).\pi_j(\lambda) \propto p(x_j|\lambda T_j,\theta_j) \pi_{j-1}(\lambda).

The next setting may be chosen to minimize expected posterior loss, maximize expected information gain, avoid a cycle slip, or satisfy a latency and bandwidth constraint. Adaptation can change θj\theta_j, TjT_j, or both.

The posterior tracks the same physical detuning at every duration, rather than treating each accumulated phase as the same unknown. The chosen setting is held fixed when differentiating its conditional likelihood; its dependence on previous outcomes is handled through the joint record.

Longer coherent phase accumulation can replace some spatial entanglement with repeated temporal queries. Heisenberg Scaling explains the ideal query scaling and its global ambiguity. Preparation, measurement, feedback latency, and branch errors determine whether that gain survives in elapsed time.

Let α\alpha be the probability of reporting one when the true state is zero, and let β\beta be the probability of reporting zero when the true state is one. If the ideal Ramsey probability is pp, the observed probability is

q=α(1−p)+(1−β)p.q = \alpha(1-p) + (1-\beta)p.

For the sine fringe,

q=12[1+α−β+(1−α−β)Csin⁡(ϕ−θ)].q = \frac12 \left[ 1+\alpha-\beta + (1-\alpha-\beta) C\sin(\phi-\theta) \right].

Readout asymmetry creates an offset; the fringe amplitude is multiplied by 1−α−β1-\alpha-\beta. Its magnitude cannot increase. If this factor is negative, relabeling the reported outcomes reverses the fringe. At quadrature the single-outcome Fisher information is

F1=(1−α−β)2C21−(α−β)2.F_1 = \frac{ (1-\alpha-\beta)^2C^2 }{ 1-(\alpha-\beta)^2 }.

For symmetric error α=β=ϵ\alpha=\beta=\epsilon, this becomes

F1=(1−2ϵ)2C2.F_1 = (1-2\epsilon)^2C^2.

Correcting a fitted contrast by a calibrated readout fidelity can estimate the premeasurement state, but it does not restore information lost by the actual detector. A state-characterization claim and an achieved sensor-sensitivity claim therefore answer different physical questions.

Contrast CC, offset bb, analysis-phase drift, and coupling calibration are often inferred jointly with the signal. For parameters ϑ=(ϕ,C,b,…)\boldsymbol\vartheta=(\phi,C,b,\ldots), the Fisher matrix is

[F(ϑ)]ab=∑xp(x∣ϑ) ∂aln⁡p ∂bln⁡p.[F(\boldsymbol\vartheta)]_{ab} = \sum_x p(x|\boldsymbol\vartheta) \, \partial_a\ln p \, \partial_b\ln p.

When the joint Fisher matrix is invertible and the estimator is locally unbiased with respect to both signal and nuisance directions, the bound is

Var⁡(ϕ^)≥[F−1]ϕϕ,\operatorname{Var}(\widehat\phi) \ge [F^{-1}]_{\phi\phi},

not 1/Fϕϕ1/F_{\phi\phi}. A single binary setting supplies a rank-one Fisher matrix and cannot identify several unconstrained parameters. Additional analysis phases or calibration measurements must provide the missing information; their shots and elapsed time also count.

The contrast function is an averaged coherence,

C(T)=∣⟨eiδϕ(T)⟩∣,C(T) = \left| \left\langle e^{i\delta\phi(T)} \right\rangle \right|,

where δϕ\delta\phi is random phase accumulated from uncontrolled fields or frequency fluctuations. Exponential contrast often indicates approximately Markovian dephasing, while Gaussian decay commonly arises from quasistatic or inhomogeneous detuning. The envelope alone rarely identifies a unique microscopic noise process.

For a stationary classical frequency noise δω(t)\delta\omega(t), the phase variance can be expressed through a filter function. With

Y(ω)=∫0Ty(t)eiωt dt,Y(\omega) = \int_0^T y(t)e^{i\omega t} \,dt,

Take the two-sided angular-frequency spectrum Sδω(ω)=∫−∞∞dt eiωt⟨δω(t)δω(0)⟩S_{\delta\omega}(\omega)=\int_{-\infty}^{\infty}dt\, e^{i\omega t}\langle\delta\omega(t)\delta\omega(0)\rangle. For zero-mean stationary Gaussian noise and a deterministic y(t)y(t),

C(T)=exp⁡[−12∫−∞∞dω2πSδω(ω)∣Y(ω)∣2].C(T) = \exp\left[ -\frac12 \int_{-\infty}^{\infty} \frac{d\omega}{2\pi} S_{\delta\omega}(\omega) |Y(\omega)|^2 \right].

Ordinary Ramsey evolution has

∣Y(ω)∣2=4sin⁡2(ωT/2)ω2,|Y(\omega)|^2 = \frac{ 4\sin^2(\omega T/2) }{ \omega^2 },

so it is strongly sensitive to quasistatic and low-frequency detuning. Echo and dynamical-decoupling sequences alter y(t)y(t) and shift sensitivity toward selected nonzero frequencies; they answer a different sensing question.

Common-mode phase noise also invalidates naive independent-probe scaling. If all NN probes share an unobserved phase δ\delta, then

P(K∣ϕ)=∫dδ P(δ)Bin⁡[K;N,p(ϕ+δ)].P(K|\phi) = \int d\delta\, P(\delta) \operatorname{Bin} \left[ K;N,p(\phi+\delta) \right].

Outcomes are conditionally independent at fixed δ\delta but correlated after δ\delta is marginalized. Increasing NN can suppress projection noise while leaving a common oscillator or environmental floor unchanged. Likewise, dead-time aliasing can fold oscillator noise into a clock measurement even when each Ramsey shot is otherwise ideal.

Ramsey interrogation is not restricted to independent qubits. For a collective spin, the first operation prepares a transverse mean spin, the signal rotates it, and the final analysis maps a transverse component to a population difference. A spin-squeezed input can reduce readout noise while retaining signal slope. Its local phase variance is

(Δϕ)2=ξR2N(\Delta\phi)^2 = \frac{\xi_R^2}{N}

for an aligned ideal readout. The contrast, squeezed variance, cycle time, and detector noise must all refer to the same operating sequence. Spin Squeezing develops the collective covariance, preparation, and entanglement criteria.

An ideal NN-qubit GHZ state,

∣GHZN⟩=∣0⟩⊗N+∣1⟩⊗N2,|\mathrm{GHZ}_N\rangle = \frac{ |0\rangle^{\otimes N} + |1\rangle^{\otimes N} }{\sqrt2},

accumulates the amplified phase NϕN\phi. A parity-like readout can have

p(1∣ϕ)=12[1+CNsin⁡(Nϕ−θ)],p(1|\phi) = \frac12 \left[ 1+C_N\sin(N\phi-\theta) \right],

and local Fisher information

Fϕ=CN2N2F_\phi = C_N^2N^2

at quadrature. The same factor NN reduces the state-phase period to 2π/N2\pi/N; two analysis phases are still needed to resolve the reflection ambiguity of a single sine fringe within that period. Independent dephasing can make CNC_N decay rapidly with NN and TT. Under independent Markovian dephasing with no preparation dead time, maximally entangled probes need not improve the asymptotic frequency resolution over optimized uncorrelated Ramsey spectroscopy.

Entanglement can still improve constants, finite-resource performance, or operation under structured noise. The defensible question is not whether the input is entangled, but whether the complete protocol improves the declared loss under the same time, probe, prior, bandwidth, and success conditions.

The Ramsey information structure is portable, but each platform supplies a different phase response and noise model.

Task Encoded phase Essential calibration Common limiting noise
Frequency comparison ϕ=(ω0−ωLO)T\phi=(\omega_0-\omega_{\mathrm{LO}})T interrogation time and oscillator phase local-oscillator noise, dead time, collisions
DC magnetometry ϕ=γBT\phi=\gamma BT gyromagnetic ratio and field projection T2∗T_2^* dephasing, field drift, readout noise
Electric-field sensing ϕ=∫ΔωE(t)dt\phi=\int\Delta\omega_E(t)dt Stark response and field geometry electric-field noise, level mixing, calibration drift
Inertial phase readout platform-dependent action phase scale factor, timing, trajectory vibration, laser phase, wave-front error
Qubit calibration ϕ=δωT+ϕc\phi=\delta\omega T+\phi_c pulse phase and timing control drift, leakage, correlated phase noise

For a spin with Hamiltonian

HB=ℏγB2σz,H_B = \frac{\hbar\gamma B}{2} \sigma_z,

the phase is ϕ=γBT\phi=\gamma BT. The projection-noise-limited field sensitivity per square root bandwidth is

ηB≥Tc∣γ∣C(T)TN.\eta_B \ge \frac{ \sqrt{T_c} }{ |\gamma| C(T)T\sqrt N }.

This formula is useful only after specifying whether NN counts simultaneous probes, repeated probes, detected probes, or accepted probes. Spatial resolution, standoff distance, sensor volume, and invasiveness can be as important as field sensitivity in an application.

1. Shared phase noise differs from independent dephasing

Section titled “1. Shared phase noise differs from independent dephasing”

Let every probe in a shot experience the same δ∼N(0,σ2)\delta\sim\mathcal N(0,\sigma^2) and let p(1∣ϕ,δ)=[1+sin⁡(ϕ+δ)]/2p(1|\phi,\delta)=[1+\sin(\phi+\delta)]/2. Find Var⁡(K)\operatorname{Var}(K) at ϕ=0\phi=0 and the variance of the locally unbiased estimator (2K/N−1)/C(2K/N-1)/C, where C=e−σ2/2C=e^{-\sigma^2/2}.

Solution

The marginal mean probability is 1/21/2. Its conditional variation has

Var⁡δ(p)=14E[sin⁡2δ]=1−e−2σ28.\operatorname{Var}_\delta(p) =\frac14\mathbb E[\sin^2\delta] =\frac{1-e^{-2\sigma^2}}8.

By total variance for K∣δ∼Binomial⁡(N,p)K|\delta\sim\operatorname{Binomial}(N,p),

Var⁡(K)=N4+N(N−1)1−e−2σ28.\operatorname{Var}(K) =\frac N4+N(N-1)\frac{1-e^{-2\sigma^2}}8.

Consequently,

Var⁡(ϕ^)=eσ2N+(1−1N)sinh⁡(σ2).\operatorname{Var}(\widehat\phi) =\frac{e^{\sigma^2}}{N} +\left(1-\frac1N\right)\sinh(\sigma^2).

The large-NN variance floor is sinh⁡(σ2)≃σ2\sinh(\sigma^2)\simeq\sigma^2 for small phase noise. Independent phase errors with the same marginal contrast would instead give eσ2/Ne^{\sigma^2}/N. A contrast measurement alone cannot distinguish these joint noise models.

NN independent probes are operated at quadrature with known contrast CC. Let f=K/Nf=K/N. Show that

ϕ^=2f−1C\widehat\phi = \frac{2f-1}{C}

is locally unbiased at ϕ=0\phi=0 and find its variance there.

Solution

Near zero,

E[f]=12(1+Csin⁡ϕ)≃12(1+Cϕ).\mathbb E[f] = \frac12(1+C\sin\phi) \simeq \frac12(1+C\phi).

Therefore

E[ϕ^]≃ϕ.\mathbb E[\widehat\phi] \simeq \phi.

At ϕ=0\phi=0, p=1/2p=1/2 and

Var⁡(f)=p(1−p)N=14N.\operatorname{Var}(f) = \frac{p(1-p)}{N} = \frac{1}{4N}.

Thus

Var⁡(ϕ^)=4C2Var⁡(f)=1NC2.\operatorname{Var}(\widehat\phi) = \frac{4}{C^2} \operatorname{Var}(f) = \frac{1}{NC^2}.

3. Optimal time under exponential dephasing

Section titled “3. Optimal time under exponential dephasing”

Assume negligible dead time and

C(T)=e−T/T2∗.C(T)=e^{-T/T_2^*}.

Find the interrogation time that maximizes frequency Fisher information per unit time.

Solution

The information per cycle is proportional to C(T)2T2C(T)^2T^2. With cycle time TT, the information rate is proportional to

R(T)=Te−2T/T2∗.R(T) = Te^{-2T/T_2^*}.

Its logarithmic derivative is

ddTln⁡R=1T−2T2∗.\frac{d}{dT}\ln R = \frac1T - \frac{2}{T_2^*}.

The maximum occurs at

Topt=T2∗2.T_{\mathrm{opt}} = \frac{T_2^*}{2}.

Maximizing single-shot information instead would give T=T2∗T=T_2^*, showing why the time objective must be stated.

Take symmetric state-classification error α=β=ϵ=0.05\alpha=\beta=\epsilon=0.05 and intrinsic contrast C=0.8C=0.8. Find the observed contrast and one-outcome Fisher information at quadrature.

Solution

Symmetric confusion multiplies contrast by 1−2ϵ1-2\epsilon, so

Cobs=(1−2ϵ)C=0.9×0.8=0.72.C_{\mathrm{obs}} = (1-2\epsilon)C = 0.9\times0.8 = 0.72.

At quadrature,

F1=Cobs2=0.5184.F_1 = C_{\mathrm{obs}}^2 = 0.5184.

Correcting the contrast can infer the state before readout, but the detector still extracts only this smaller amount of information per outcome.

A Ramsey experiment uses T=20 msT=20\,\mathrm{ms}. By how much can angular frequency change while producing the same ideal fringe? Give the corresponding ordinary-frequency spacing.

Solution

The fringe is unchanged when

δωT⟶δωT+2πm.\delta\omega T \longrightarrow \delta\omega T+2\pi m.

Adjacent angular-frequency aliases are separated by

Δωalias=2πT=100π rad s−1.\Delta\omega_{\mathrm{alias}} = \frac{2\pi}{T} = 100\pi\,\mathrm{rad\,s^{-1}}.

The ordinary-frequency spacing is

Δfalias=1T=50 Hz.\Delta f_{\mathrm{alias}} = \frac{1}{T} = 50\,\mathrm{Hz}.

Two protocols have the same NN, contrast, and interrogation time TT. Protocol A has no dead time, while protocol B has td=3Tt_{\mathrm d}=3T. Compare their frequency standard deviations after the same wall-clock averaging time.

Solution

The variance scales with cycle time Tc=T+tdT_c=T+t_{\mathrm d}. Hence

Δδω^BΔδω^A=Tc,BTc,A=4TT=2.\frac{ \Delta\widehat{\delta\omega}_B }{ \Delta\widehat{\delta\omega}_A } = \sqrt{ \frac{T_{c,B}}{T_{c,A}} } = \sqrt{ \frac{4T}{T} } = 2.

Protocol B has twice the standard deviation after equal wall-clock time, despite identical one-shot statistics.

Compare an ideal NN-qubit GHZ Ramsey fringe with an independent-probe fringe. What happens to local Fisher information and the state-phase period?

Solution

At quadrature and unit contrast, the GHZ fringe depends on NϕN\phi, so

Fϕ,GHZ=N2.F_{\phi,\mathrm{GHZ}} = N^2.

NN independent probes give total information NN. The GHZ state therefore has an ideal factor-NN local information gain for the same simultaneous probe count. Its fringe period is

2πN,\frac{2\pi}{N},

instead of 2π2\pi. The local gain is accompanied by a factor-NN reduction in phase period, before including GHZ preparation cost or faster decoherence. A single sine measurement also has a reflection ambiguity within its period; a second analysis phase resolves that ambiguity.

An ensemble of N=104N=10^4 independent spins has γ=2π×28 GHz T−1\gamma=2\pi\times28\,\mathrm{GHz\,T^{-1}}, T=1 μsT=1\,\mu\mathrm{s}, C=0.7C=0.7, and Tc=5 μsT_c=5\,\mu\mathrm{s}. Estimate the projection-noise-limited ηB\eta_B.

Solution

Use

ηB=TcγCTN.\eta_B = \frac{\sqrt{T_c}}{\gamma CT\sqrt N}.

Substitution gives

ηB=5×10−6 s(2π)(28×109 s−1T−1)(0.7)(10−6 s)(100)≃1.8×10−10 T Hz−1/2.\begin{aligned} \eta_B &= \frac{ \sqrt{5\times10^{-6}\,\mathrm s} }{ (2\pi)(28\times10^9\,\mathrm{s^{-1}T^{-1}}) (0.7)(10^{-6}\,\mathrm s)(100) } \\ &\simeq 1.8\times10^{-10} \,\mathrm{T\,Hz^{-1/2}}. \end{aligned}

This is about 180 pT Hz−1/2180\,\mathrm{pT\,Hz^{-1/2}}. It is a model benchmark, not a complete instrument sensitivity: calibration noise, spatial response, technical phase noise, and long-term drift are absent.

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