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Quantum Estimation for Magnetometry

A magnetometer estimates a specified property of a magnetic field from a physical response. In quantum magnetometry, that response is encoded in a quantum state or quantum dynamical process before a measurement produces classical data. The phrase “magnetic-field sensitivity” is incomplete until the field component, spatial weighting, temporal waveform, bandwidth, averaging convention, dynamic range, and operating conditions are stated.

Required background. Parameter estimation, Fisher information, and Ramsey interferometry supply the likelihood and readout. Spin in magnetic fields defines the signed magnetic coupling.

For optical pumping, SERF operation, coil calibration, and instrument systematics, see AMO Magnetometry.

A magnetic field is a vector field over space and time. A useful experiment rarely estimates all of it. Instead, it estimates one or several parameters in a model such as

B(r,t)=B0(r,t)+b s(t)u(r)+∑aνa sa(t)ua(r).\mathbf B(\mathbf r,t) = \mathbf B_0(\mathbf r,t) + b\,s(t)\mathbf u(\mathbf r) + \sum_a \nu_a\, s_a(t)\mathbf u_a(\mathbf r).

Here bb is the target parameter, s(t)u(r)s(t)\mathbf u(\mathbf r) is its known spatiotemporal mode, and the νa\nu_a are nuisance parameters. Depending on the task, bb might be

  • a static field component at a calibrated location;
  • the amplitude and phase of a sinusoidal field;
  • a gradient or difference between two regions;
  • a Fourier coefficient in a prescribed bandwidth;
  • a source parameter inferred through a field model; or
  • a stochastic quantity such as a power spectral density.

These are different statistical problems. A protocol optimized for a known sinusoid can reject a static offset and yet be a poor broadband magnetometer. A gradiometer can reject uniform environmental noise while being deliberately insensitive to the common field. A relaxometry experiment estimates noise near a transition frequency rather than a deterministic field amplitude.

A sensitivity must therefore be attached to a field model and an observation model, rather than only to the name of the instrument.

Magnetic Coupling as a Parameter Generator

Section titled “Magnetic Coupling as a Parameter Generator”

Let a controlled sensor couple to an effective field component through

HB(t)=−ℏγB(t)G,H_B(t) = -\hbar\gamma B(t)G,

where γ\gamma is the signed gyromagnetic ratio and GG is a dimensionless generator. For a spin-1/21/2 sensor with quantization axis zz, G=σz/2G=\sigma_z/2. For NN spins responding collectively,

G=Jz=12∑k=1Nσz(k).G=J_z = \frac12\sum_{k=1}^{N}\sigma_z^{(k)}.

Suppose control pulses produce a toggling function y(t)y(t) and the target field is B(t)=b s(t)B(t)=b\,s(t). If the effective generators commute at different times, the parameter-dependent unitary is

Ub=exp⁡ ⁣(iγbAG),A=∫0Ty(t)s(t) dt.U_b = \exp\!\left(i\gamma b\mathcal A G\right), \qquad \mathcal A = \int_0^T y(t)s(t)\,dt.

The overlap A\mathcal A is the temporal signal gain. For a static field and free precession, s(t)=y(t)=1s(t)=y(t)=1 and A=T\mathcal A=T. A spin echo has equal positive and negative lobes, so it rejects a static field but can acquire phase from an alternating field synchronized to the sign changes.

For a pure input state, the quantum Fisher information (QFI) for bb is

Fb(Q)=4γ2A2 (ΔG)2.F_b^{(Q)} = 4\gamma^2\mathcal A^2 \,(\Delta G)^2.

This equation separates three ingredients:

  1. the coupling strength ∣γ∣|\gamma|;
  2. the temporal overlap ∣A∣|\mathcal A|; and
  3. the generator variance supplied by the probe state.

It is a local information measure for the specified parameter model. It does not by itself state the capture range, identify a realizable measurement, include cycle overhead, or guarantee robustness to nuisance fields.

Ramsey-like preparation and readout often produce a binary outcome x∈{+1,−1}x\in\{+1,-1\} with likelihood

p(x∣b)=12[1+xCsin⁡(γbA+θ)].p(x\mid b) = \frac12 \left[ 1+xC\sin(\gamma b\mathcal A+\theta) \right].

The analysis phase θ\theta selects the working point. With the signed Hamiltonian above, one compatible qubit measurement is Ex=[I+x(sin⁡θ σx−cos⁡θ σy)]/2E_x=[I+x(\sin\theta\,\sigma_x-\cos\theta\,\sigma_y)]/2 on an initially +x+x-polarized state. This fixes the sign of the displayed sine fringe.

The effective contrast 0≤C≤10\le C\le1 can describe independent dephasing and symmetric readout errors. Asymmetric classification requires an offset as well. Here CC is treated as known and independent of bb. The classical Fisher information is

Fb=C2γ2A2cos⁡2(γbA+θ)1−C2sin⁡2(γbA+θ).F_b = \frac{ C^2\gamma^2\mathcal A^2 \cos^2(\gamma b\mathcal A+\theta) }{ 1-C^2\sin^2(\gamma b\mathcal A+\theta) }.

At quadrature, where the sine term vanishes,

Fb=C2γ2A2.F_b = C^2\gamma^2\mathcal A^2.

For NN independent, identically coupled spins read out in one cycle, the information adds. A shared random field must first be included in their joint likelihood; averaging it into the single-spin contrast does not preserve independence:

Fb,N=NC2γ2A2.F_{b,N} = NC^2\gamma^2\mathcal A^2.

The same scaling follows from the QFI. An equatorial coherent spin state has (ΔJz)2=N/4(\Delta J_z)^2=N/4, giving

Fb(Q)=Nγ2A2F_b^{(Q)} = N\gamma^2\mathcal A^2

before contrast loss. Equality between a measurement’s classical Fisher information and the QFI requires the appropriate state, working point, and readout; quoting QFI alone does not establish experimental sensitivity.

Sensitivity Means Information per Wall Time

Section titled “Sensitivity Means Information per Wall Time”

Let the complete cycle last

Tc=T+tprep+tread+treset.T_c = T+t_{\mathrm{prep}}+t_{\mathrm{read}}+t_{\mathrm{reset}}.

For statistically independent cycles at a fixed working point, the Fisher information rate is

F˙b=NC2γ2A2Tc.\dot F_b = \frac{NC^2\gamma^2\mathcal A^2}{T_c}.

The corresponding local Cramér–Rao sensitivity coefficient is

ηB≡1F˙b=TcC∣γ∣ ∣A∣N.\eta_B \equiv \frac{1}{\sqrt{\dot F_b}} = \frac{\sqrt{T_c}} {C|\gamma|\,|\mathcal A|\sqrt N}.

For free-precession DC sensing, A=T\mathcal A=T. Under the assumptions above, an averaging time τ=mTc\tau=mT_c gives

δb(τ)≥ηBτ.\delta b(\tau) \ge \frac{\eta_B}{\sqrt\tau}.

The units of ηB\eta_B are T/Hz\mathrm{T}/\sqrt{\mathrm{Hz}}. It was defined here by δbτ\delta b\sqrt{\tau}. For a continuous white-noise record with unit DC response, a rectangular average has Var⁡(bˉ)=SB(1)(0)/(2τ)\operatorname{Var}(\bar b)=S_B^{(1)}(0)/(2\tau) when SB(1)S_B^{(1)} is a one-sided PSD per hertz. Thus the corresponding one-sided amplitude spectral density is 2 ηB\sqrt2\,\eta_B, rather than ηB\eta_B. The averaging filter and spectral convention fix this conversion.

Dead time matters twice. It reduces the number of trials per unit time, and it can expose a pulsed sensor to aliasing of environmental or local-oscillator noise. Rejected cycles, preparation failures, recalibration, and recovery from saturation belong in TcT_c or in a separately reported duty factor.

Consider N=106N=10^6 independent spins with

∣γ∣2π=7 GHz/T,T=1 ms,C=0.70,Tc=2 ms.\frac{|\gamma|}{2\pi} = 7\,\mathrm{GHz/T}, \qquad T=1\,\mathrm{ms}, \qquad C=0.70, \qquad T_c=2\,\mathrm{ms}.

For a static field, A=T\mathcal A=T, so the ideal projection-noise benchmark is

ηB=2×10−30.70(2π)(7×109)(10−3)106≃1.45×10−12 T/Hz.\begin{aligned} \eta_B &= \frac{\sqrt{2\times10^{-3}}} {0.70(2\pi)(7\times10^9)(10^{-3})\sqrt{10^6}} \\ &\simeq 1.45\times10^{-12} \ \mathrm{T}/\sqrt{\mathrm{Hz}}. \end{aligned}

This is not yet an instrument specification. It omits technical readout noise, field calibration, spatial averaging, correlated cycles, estimator loss, dynamic range, and uptime. Its value is that it states a transparent reference against which the complete device can be compared.

Write the field along the sensed axis as

B(t)=b s(t)+ξB(t),B(t)=b\,s(t)+\xi_B(t),

where s(t)s(t) is a deterministic target waveform and ξB(t)\xi_B(t) is stationary zero-mean magnetic noise. The accumulated phase is

ϕ=γbA+γ∫0Ty(t)ξB(t) dt.\phi = \gamma b\mathcal A + \gamma\int_0^T y(t)\xi_B(t)\,dt.

The control modulation y(t)y(t) is therefore both a signal template and a noise filter. Define

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

For a sinusoidal signal s(t)=cos⁡(ωst+φs)s(t)=\cos(\omega_s t+\varphi_s),

A=Re⁡[eiφsY(ωs)].\mathcal A = \operatorname{Re} \left[ e^{i\varphi_s}Y(\omega_s) \right].

With the two-sided power spectral density convention

⟨ξ~B(ω)ξ~B∗(ω′)⟩=2πδ(ω−ω′)SB(ω),\left\langle \widetilde\xi_B(\omega) \widetilde\xi_B^*(\omega') \right\rangle = 2\pi\delta(\omega-\omega')S_B(\omega),

the phase variance is

Var⁡(ϕn)=γ2∫−∞∞dω2πSB(ω)∣Y(ω)∣2.\operatorname{Var}(\phi_{\mathrm n}) = \gamma^2 \int_{-\infty}^{\infty} \frac{d\omega}{2\pi} S_B(\omega)|Y(\omega)|^2.

For Gaussian phase noise, the coherence is

C(T)=e−χ(T),χ(T)=12Var⁡(ϕn).C(T)=e^{-\chi(T)}, \qquad \chi(T) = \frac12\operatorname{Var}(\phi_{\mathrm n}).

Different spectral conventions move factors of two between SBS_B, χ\chi, and the integration range. The physical prediction is unchanged if one convention is used consistently.

For one ideal echo pulse at T/2T/2, y(t)=+1y(t)=+1 in the first half and −1-1 in the second. Comparing its Fourier transform with free Ramsey precession gives

∣YR(ω)∣2=4sin⁡2(ωT/2)ω2,∣YE(ω)∣2=16sin⁡4(ωT/4)ω2.\begin{aligned} |Y_{\mathrm R}(\omega)|^2 &=\frac{4\sin^2(\omega T/2)}{\omega^2},\\ |Y_{\mathrm E}(\omega)|^2 &=\frac{16\sin^4(\omega T/4)}{\omega^2}. \end{aligned}

The zero-frequency limits are T2T^2 and zero. For the known signal s(t)=sin⁡(2πt/T)s(t)=\sin(2\pi t/T), Ramsey gives A=0\mathcal A=0 and echo gives A=2T/π\mathcal A=2T/\pi.

Echo modulation matched to an alternating signal, with exact Ramsey and echo frequency responses

(a) One echo pulse reverses the sign of the interaction, making both halves of the sinusoidal signal add to the accumulated phase. (b) The exact normalized filters show the cost: echo rejects a constant field while retaining nonzero-frequency response. The waveform phase matters as well as the filter magnitude; a shifted sinusoid can have a different overlap.

Filter matching has a hard limitation: control cannot reject noise that is indistinguishable from the signal in the same spatiotemporal mode. More pulses can suppress low-frequency noise while sharpening an AC passband, but pulse errors, finite pulse duration, timing jitter, harmonics, and reduced duty factor can erase the expected gain. The ideal Y(ω)Y(\omega) and the measured transfer function should both be reported.

Coherence and the Optimal Interrogation Time

Section titled “Coherence and the Optimal Interrogation Time”

Longer interrogation increases phase gain, but it usually reduces contrast. For a phenomenological stretched-exponential envelope with p>0p>0,

C(T)=exp⁡ ⁣[−(T/T2)p],C(T) = \exp\!\left[-(T/T_2)^p\right],

where T2T_2 refers to the actual DC interrogation (often denoted T2∗T_2^* for free precession, not the longer echo coherence time), the information rate with negligible overhead is

F˙b(T)=Nγ2Texp⁡ ⁣[−2(T/T2)p].\dot F_b(T) = N\gamma^2T \exp\!\left[-2(T/T_2)^p\right].

Its optimum satisfies

T∗=T2(12p)1/p.T_* = T_2 \left(\frac{1}{2p}\right)^{1/p}.

With fixed dead time tdt_d, the rate becomes

F˙b(T)=Nγ2T2e−2(T/T2)pT+td,\dot F_b(T) = \frac{ N\gamma^2T^2e^{-2(T/T_2)^p} }{T+t_d},

and the stationary condition is

2T−2pTp−1T2p−1T+td=0.\frac2T - \frac{2pT^{p-1}}{T_2^p} - \frac1{T+t_d} =0.

This optimization is local and model-dependent. Phase wrapping may force a shorter TT; overhead can favor a longer TT; colored noise can invalidate the stretched-exponential model; and adaptive multi-time protocols can combine a wide capture range with a long final interrogation.

A single sensitivity number hides the sensor transfer function. At minimum, one should distinguish

  • interrogation bandwidth: the width of the temporal filter around its target frequency;
  • sampling bandwidth: limited by cycle time and irregular dead time;
  • closed-loop bandwidth: relevant when feedback tracks a field;
  • analysis bandwidth: imposed by the estimator or reported spectrum; and
  • usable bandwidth: the region over which calibration, linearity, and noise are validated.

The binary likelihood is periodic in phase. For one interrogation, fields separated by

Δbalias=2π∣γA∣\Delta b_{\mathrm{alias}} = \frac{2\pi}{|\gamma\mathcal A|}

produce the same ideal probability. A roughly linear single-fringe interval is smaller still. Increasing TT improves local sensitivity while reducing unambiguous range. Bias fields, quadrature readout, multiple interrogation times, adaptive control, and an independent coarse channel can resolve aliases, but those resources belong in the protocol description.

For a continuously operated linear sensor, it is often clearer to write

m(ω)=χMB(ω)Beff(ω)+nM(ω),m(\omega) = \chi_{MB}(\omega)B_{\mathrm{eff}}(\omega) + n_M(\omega),

where mm is the measured output and χMB\chi_{MB} is the calibrated complex response. Output noise referred to the input gives

SBeq(ω)=SM(ω)∣χMB(ω)∣2.S_B^{\mathrm{eq}}(\omega) = \frac{S_M(\omega)}{|\chi_{MB}(\omega)|^2}.

An amplitude spectral density SBeq\sqrt{S_B^{\mathrm{eq}}} has units T/Hz\mathrm{T}/\sqrt{\mathrm{Hz}}; the PSD has units T2/Hz\mathrm{T}^2/\mathrm{Hz}; and a one-shot standard deviation has units T\mathrm T. These quantities should not be interchanged.

Real sensors average the field over a finite region. A scalar channel can be modeled as

Beff(t)=∫d3r w(r)n(r)⋅B(r,t),∫d3r w(r)=1.B_{\mathrm{eff}}(t) = \int d^3r\, w(\mathbf r) \mathbf n(\mathbf r)\cdot \mathbf B(\mathbf r,t), \qquad \int d^3r\,w(\mathbf r)=1.

The kernel w(r)w(\mathbf r) includes sensor density, optical intensity, mode overlap, collection efficiency, and analysis weighting. The local sensitive axis is n(r)\mathbf n(\mathbf r). Two devices with the same field-noise floor can have very different value for a localized source because their active volumes, standoff distances, and kernels differ.

Spatial resolution is not simply the physical sensor size. It also depends on source distance, field propagation, channel geometry, inversion priors, and regularization. For a multi-channel array,

Bi(t)=∫d3r Ki(r)⋅Js(r,t)+ni(t),B_i(t) = \int d^3r\, \mathbf K_i(\mathbf r)\cdot \mathbf J_s(\mathbf r,t) +n_i(t),

where Js\mathbf J_s denotes a source distribution and Ki\mathbf K_i is a forward kernel. Estimating the source is then an inverse problem, not merely a collection of independent field estimates. Cross-channel covariance and uncertainty in the kernels must enter the inference.

A gradiometer estimates a difference such as

gB=B1−B2d.g_B = \frac{B_1-B_2}{d}.

Common-mode rejection depends on matched gains, axes, transfer functions, and timing. A low differential noise floor does not establish the absolute noise of either channel.

Vector Magnetometry Is Multiparameter Estimation

Section titled “Vector Magnetometry Is Multiparameter Estimation”

For a spin coupled to all three components,

HB=−ℏγ(BxJx+ByJy+BzJz).H_B = -\hbar\gamma \left( B_xJ_x+B_yJ_y+B_zJ_z \right).

At zero field, the pure-state QFI matrix is

Fμν(Q)=4γ2T2Cov⁡s(Jμ,Jν),F_{\mu\nu}^{(Q)} =4\gamma^2T^2\operatorname{Cov}_{\mathrm s}(J_\mu,J_\nu),

where Cov⁡s(A,B)=⟨{A,B}⟩/2−⟨A⟩⟨B⟩\operatorname{Cov}_{\mathrm s}(A,B)=\langle\{A,B\}\rangle/2-\langle A\rangle\langle B\rangle. This expression also gives the leading short-time result. At an arbitrary nonzero bias, the noncommuting rotations require the exact local generators

Kμ=iU†∂BμU=−γ∫0TU†(t)JμU(t) dt,Fμν(Q)=4Cov⁡s(Kμ,Kν),K_\mu=iU^\dagger\partial_{B_\mu}U =-\gamma\int_0^T U^\dagger(t)J_\mu U(t)\,dt, \qquad F_{\mu\nu}^{(Q)}=4\operatorname{Cov}_{\mathrm s}(K_\mu,K_\nu),

with expectations in the input state. Simply replacing KμK_\mu by −γTJμ-\gamma TJ_\mu can give the wrong information at finite bias; Exercise 8 gives an explicit counterexample. For a single pure qubit and one fixed preparation the QFI matrix for three field components is also rank deficient: the output state has only two independent real coordinates. Different preparations, controls, or larger probes can provide additional identifiable directions.

Unlike three unrelated scalar parameters, the field components are generated by noncommuting observables. Measurements that are optimal for different components need not be jointly compatible. The matrix quantum Cramér–Rao bound may therefore be unattainable by one measurement, even though each diagonal entry is attainable in a separate experiment.

Practical vector sensors address this by using distinct orientations, independent subensembles, sequential settings, controlled bias fields, or a joint measurement designed for a weighted cost. The resource split must be visible: three subensembles containing N/3N/3 sensors do not each inherit the NN-sensor scalar benchmark.

Nuisance fields also reduce information. If bb is the target and ν\boldsymbol\nu collects unknown nuisance parameters, then for a classical Fisher matrix with invertible nuisance block, the effective local information is the Schur complement

Fb,eff=Fbb−FbνFνν−1Fνb.F_{b,\mathrm{eff}} = F_{bb} - F_{b\nu} F_{\nu\nu}^{-1} F_{\nu b}.

Calibration data or prior information can improve this quantity, but they are then resources in the inference. Treating unknown transverse fields as known can make a scalar sensitivity estimate unrealistically optimistic.

For independent spins, generator variances add and the local QFI scales as NN. This is the standard quantum limit for the matched preparation, interrogation, readout, and wall-time resources. Quantum correlations can change the variance or the accessible measurement noise.

For a collective spin used as a small-angle sensor, the Wineland parameter

ξR2=N(ΔJ⊥)2∣⟨J⟩∣2\xi_R^2 = \frac{N(\Delta J_\perp)^2} {|\langle\mathbf J\rangle|^2}

gives an ideal phase variance

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

Thus ξR2<1\xi_R^2<1 gives a local gain over the unit-contrast coherent-spin reference. This parameter includes the surviving mean-spin response; inhomogeneous coupling may require a modified reference. Information per elapsed time must additionally include preparation and readout time, failed trials, and the noise of the actual detector. Noise reduction in a detector quadrature without a calibrated signal response is not sufficient.

An ideal GHZ-like state has (ΔG)2∝N2(\Delta G)^2\propto N^2 and can achieve local QFI proportional to N2N^2. It also produces a fringe NN times narrower, reducing the prior range, and is fragile to loss and dephasing. Under independent Markovian dephasing, optimizing interrogation time commonly removes the asymptotic scaling advantage even though finite-NN gains may remain. Claims about Heisenberg scaling must specify the noise model and count sequential queries, preparation, ancillas, control, and repetitions.

Measurement backaction and conditional gain

Section titled “Measurement backaction and conditional gain”

Continuous or repeated nondemolition readout can conditionally squeeze an ensemble and track a field at the same time. Probe photons or auxiliary modes then contribute imprecision, backaction, decoherence, and sample disturbance. An in-loop record can look quieter because feedback suppresses the measured quantity. Independent or out-of-loop validation is needed to show that the field estimate itself improved.

The strongest comparison is end to end: the quantum protocol and its best classical reference use the same sensing particles, active volume, total time, bandwidth, field mode, prior range, calibration information, accepted trials, and disturbance budget.

Field sensitivity alone favors large sensing volumes. A common cross-platform normalization is the magnetic energy resolution per bandwidth

ER=SBV2μ0,E_R = \frac{S_B V}{2\mu_0},

Here take SBS_B to be a one-sided field-noise PSD per hertz and VV an effective sensor volume; numerical comparisons must use that same convention. Its units are energy times time, or action. The expression is motivated by the magnetic energy density B2/(2μ0)B^2/(2\mu_0).

This metric can reveal tradeoffs hidden by a bare field-noise floor, and many sensor classes operate near scales of order ℏ\hbar. It is not a universal single-number ranking or a geometry-free quantum limit. The appropriate VV, spectral convention, measured component, bandwidth, demagnetizing geometry, coupling efficiency, and standoff must be defined. A nanoscale sensor and a large-volume ensemble may solve different source-estimation problems even when their ERE_R values coincide.

For NN independent spins with

p(x∣b)=12[1+xCsin⁡(γbT)],p(x\mid b) = \frac12[1+xC\sin(\gamma bT)],

derive the Fisher information at b=0b=0. What one-shot bound follows?

Solution

At b=0b=0, both outcomes have probability 1/21/2, and

∂bp(x∣b)∣b=0=xCγT2.\left.\partial_b p(x\mid b)\right|_{b=0} = \frac{xC\gamma T}{2}.

The single-spin Fisher information is

Fb,1=∑x=±1(CγT/2)21/2=C2γ2T2.F_{b,1} = \sum_{x=\pm1} \frac{(C\gamma T/2)^2}{1/2} = C^2\gamma^2T^2.

Independent information adds, so

Fb,N=NC2γ2T2.F_{b,N} = NC^2\gamma^2T^2.

The local Cramér–Rao bound for one cycle is

δb≥1C∣γ∣TN.\delta b \ge \frac{1}{C|\gamma|T\sqrt N}.

Reproduce the worked benchmark for N=106N=10^6, ∣γ∣/(2π)=7 GHz/T|\gamma|/(2\pi)=7\,\mathrm{GHz/T}, T=1 msT=1\,\mathrm{ms}, C=0.70C=0.70, and Tc=2 msT_c=2\,\mathrm{ms}. What uncertainty is expected after 100 s100\,\mathrm s under the independent-cycle model?

Solution

The information-rate expression gives

ηB=1.45×10−12 T/Hz.\eta_B = 1.45\times10^{-12} \ \mathrm{T}/\sqrt{\mathrm{Hz}}.

After τ=100 s\tau=100\,\mathrm s,

δb(100 s)=ηB100≃1.45×10−13 T.\delta b(100\,\mathrm s) = \frac{\eta_B}{\sqrt{100}} \simeq 1.45\times10^{-13}\ \mathrm T.

This extrapolation assumes stationary, independent cycles and no drift floor. A real long-duration test must verify the τ−1/2\tau^{-1/2} regime.

3. Optimize stretched-exponential coherence

Section titled “3. Optimize stretched-exponential coherence”

With negligible dead time and C(T)=e−(T/T2)pC(T)=e^{-(T/T_2)^p}, derive the interrogation time that maximizes DC Fisher information per unit time. Evaluate T∗/T2T_*/T_2 for p=1p=1 and p=2p=2.

Solution

Apart from constants,

F˙b(T)∝Te−2(T/T2)p.\dot F_b(T) \propto Te^{-2(T/T_2)^p}.

The logarithmic derivative is

ddTln⁡F˙b=1T−2pTp−1T2p.\frac{d}{dT}\ln\dot F_b = \frac1T - \frac{2pT^{p-1}}{T_2^p}.

Setting it to zero gives

(T∗T2)p=12p,\left(\frac{T_*}{T_2}\right)^p = \frac1{2p},

so

T∗T2=(12p)1/p.\frac{T_*}{T_2} = \left(\frac1{2p}\right)^{1/p}.

Therefore T∗/T2=1/2T_*/T_2=1/2 for p=1p=1 and T∗/T2=1/2T_*/T_2=1/2 for p=2p=2. The equality for these two cases is coincidental.

Let

y(t)={+1,0≤t<T/2,−1,T/2≤t≤T.y(t) = \begin{cases} +1,&0\le t<T/2,\\ -1,&T/2\le t\le T. \end{cases}

Find A\mathcal A for a static signal s(t)=1s(t)=1. Then find it for a signal that changes sign at T/2T/2 in synchrony with y(t)y(t).

Solution

For the static signal,

A=∫0T/2dt−∫T/2Tdt=0.\mathcal A = \int_0^{T/2}dt - \int_{T/2}^{T}dt =0.

The echo rejects an ideal static field. For the synchronized signal s(t)=y(t)s(t)=y(t),

A=∫0Ty2(t) dt=T.\mathcal A = \int_0^T y^2(t)\,dt =T.

The same sequence can therefore reject one temporal mode and retain another. This is mode selection, not universal noise suppression.

A protocol has ∣γA∣=2π×106 T−1|\gamma\mathcal A|=2\pi\times10^6\,\mathrm{T}^{-1}. Find the field spacing between equivalent fringes. What happens to this spacing if the interrogation overlap doubles?

Solution

The alias spacing is

Δbalias=2π∣γA∣=10−6 T.\Delta b_{\mathrm{alias}} = \frac{2\pi}{|\gamma\mathcal A|} = 10^{-6}\ \mathrm T.

Doubling ∣A∣|\mathcal A| doubles the local phase response and quadruples Fisher information at fixed contrast, but halves the fringe spacing to 0.5 μT0.5\,\mu\mathrm T. The local precision improves while the unambiguous range shrinks.

The Fisher matrix for target field bb and nuisance offset ν\nu is

F=(100606050)T−2.F = \begin{pmatrix} 100&60\\ 60&50 \end{pmatrix} \mathrm T^{-2}.

Find the effective information about bb when ν\nu is unknown. Compare it with the value obtained by pretending ν\nu were known.

Solution

The Schur complement is

Fb,eff=100−60250=28 T−2.F_{b,\mathrm{eff}} = 100- \frac{60^2}{50} =28\ \mathrm T^{-2}.

The corresponding local variance bound is 1/28 T21/28\,\mathrm T^2, rather than 1/100 T21/100\,\mathrm T^2. Correlation with an unknown nuisance parameter removes most of the nominal information about bb.

A sensor has one-sided field-noise PSD SB=10−30 T2/HzS_B=10^{-30}\,\mathrm{T^2/Hz} and effective volume V=1.0 mm3V=1.0\,\mathrm{mm^3}. Estimate ER/ℏE_R/\hbar using μ0=4π×10−7 H/m\mu_0=4\pi\times10^{-7}\,\mathrm{H/m} and ℏ=1.055×10−34 J s\hbar=1.055\times10^{-34}\,\mathrm{J\,s}.

Solution

Since 1 mm3=10−9 m31\,\mathrm{mm^3}=10^{-9}\,\mathrm{m^3},

ER=10−30×10−92(4π×10−7)≃3.98×10−34 J s.E_R = \frac{10^{-30}\times10^{-9}} {2(4\pi\times10^{-7})} \simeq 3.98\times10^{-34}\ \mathrm{J\,s}.

Thus

ERℏ≃3.8.\frac{E_R}{\hbar} \simeq 3.8.

The number is meaningful only with the stated spectral and effective-volume conventions. It does not determine spatial resolution or source sensitivity.

Prepare a spin-1/21/2 in ∣+z⟩|+z\rangle and let H=−ℏγ(B0Jz+bJx)H=-\hbar\gamma(B_0J_z+bJ_x). For ω0=γB0≠0\omega_0=\gamma B_0\ne0, find the QFI for a small transverse field bb at b=0b=0.

Solution

The local generator is

Kb=−γ[sin⁡(ω0T)ω0Jx+1−cos⁡(ω0T)ω0Jy].K_b=-\gamma\left[ \frac{\sin(\omega_0T)}{\omega_0}J_x +\frac{1-\cos(\omega_0T)}{\omega_0}J_y \right].

In ∣+z⟩|+z\rangle, both transverse variances are 1/41/4 and their symmetrized covariance vanishes. Therefore

Fb(Q)=4Var⁡(Kb)=4γ2ω02sin⁡2 ⁣(ω0T2).F_b^{(Q)} =4\operatorname{Var}(K_b) =\frac{4\gamma^2}{\omega_0^2} \sin^2\!\left(\frac{\omega_0T}{2}\right).

The zero-bias limit is γ2T2\gamma^2T^2. At ω0T=2π\omega_0T=2\pi, however, the first-order information is zero: the bias rotation averages away the small transverse perturbation over a full cycle. The zero-field covariance formula would incorrectly predict γ2T2\gamma^2T^2 there.