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Atomic Clocks as Quantum Estimators

A passive atomic clock is a sequential quantum estimator wrapped around an oscillator. During each cycle, an ensemble of atoms compares the oscillator phase with a reproducible transition. A measurement converts the accumulated relative phase into data, an estimator updates the inferred oscillator state, and a controller applies a correction. The continuously available output is the disciplined oscillator, not a stream of autonomous atomic ticks.

A narrow Ramsey fringe or a small state-preparation variance is only one ingredient. The oscillator continues to drift between atomic measurements, and the controller must identify the correct fringe branch while correcting that drift. This page develops the statistical consequences of repeated interrogation; AMO Atomic Clocks develops physical clock architectures, systematic shifts, and the sensitivity-function treatment.

Required background. Parameter estimation and Fisher information provide likelihoods and local bounds; the standard quantum limit and Ramsey interferometry supply the independent-atom readout.

Atomic measurements and oscillator feedback

Section titled “Atomic measurements and oscillator feedback”

A transition with unperturbed angular frequency ω0\omega_0 provides the quantum reference. The microwave or optical oscillator carries phase continuously, while each interrogation compares its phase with the atoms. An estimator converts the outcome into an inferred frequency error, and the controller uses that error to steer the oscillator.

The atoms are excellent long-term references but are observed intermittently. The local oscillator supplies continuity but wanders. The clock is therefore a hybrid quantum–classical control system whose state is only partially observed.

An in-loop error signal can be small because feedback suppresses it. That does not independently demonstrate that the output is correct. A trustworthy clock requires a second measurement path, a comparison with another reference, or a validated model showing how the in-loop record predicts out-of-loop behavior.

Let the local oscillator have instantaneous fractional frequency offset

yLO(t)=ωLO(t)−ω0ω0.y_{\mathrm{LO}}(t) = \frac{\omega_{\mathrm{LO}}(t)-\omega_0}{\omega_0}.

During cycle jj, the interrogation sensitivity function gj(t)g_j(t) weights oscillator fluctuations. A useful relative-phase model is

ϕj=ω0∫tjtj+Tcgj(t)yLO(t) dt+ϕsys,j+ϕctrl,j.\phi_j = \omega_0 \int_{t_j}^{t_j+T_c} g_j(t)y_{\mathrm{LO}}(t)\,dt + \phi_{\mathrm{sys},j} + \phi_{\mathrm{ctrl},j}.

Here TcT_c is the full cycle time, ϕsys,j\phi_{\mathrm{sys},j} collects atomic and apparatus shifts, and ϕctrl,j\phi_{\mathrm{ctrl},j} is the known analysis or servo phase. For ideal Ramsey free evolution of duration TT, gj(t)=1g_j(t)=1 during the dark interval and zero elsewhere, so a constant detuning gives

ϕj=δωjT+ϕsys,j+ϕctrl,j.\phi_j=\delta\omega_jT+\phi_{\mathrm{sys},j} +\phi_{\mathrm{ctrl},j}.

Conditional on the phase history, NN independent two-level atoms with state-resolved population detection have a binomial excited count:

Kj∼Binomial⁡ ⁣(N,pe(ϕj)),K_j\sim\operatorname{Binomial} \!\left(N,p_e(\phi_j)\right),

with an effective Ramsey fringe

pe(ϕj)=1+Csin⁡ϕj2p_e(\phi_j) = \frac{1+C\sin\phi_j}{2}

when the analysis phase places the clock at quadrature. Here CC describes the conditional single-atom contrast, including independent dephasing or preparation imperfections. An unresolved oscillator phase shared by the atoms must instead be marginalized over the whole binomial likelihood; it correlates their outcomes. Replacing it by a reduced marginal contrast does not preserve independent-binomial statistics. Detection errors likewise require a response model.

The atomic outcome is not a direct observation of instantaneous frequency. It is a noisy, periodic observation of an integrated phase. This distinction is central to clock design.

For one atom with the quadrature likelihood above, the phase FI is C2C^2 at ϕ=0\phi=0. For NN independent atoms,

FϕCSS=NC2,F_\phi^{\mathrm{CSS}} = NC^2,

where CSS denotes a coherent spin state. Since ϕ=δωT\phi=\delta\omega T, information transforms as

FδωCSS=NC2T2.F_{\delta\omega}^{\mathrm{CSS}} = NC^2T^2.

If independent cycles of duration TcT_c can be combined and the oscillator model does not introduce an additional limit, the information rate is

F˙δω=NC2T2Tc.\dot F_{\delta\omega} = \frac{NC^2T^2}{T_c}.

Writing the duty factor as D=T/TcD=T/T_c gives

F˙δω=NC2TD.\dot F_{\delta\omega} = NC^2TD.

This formula makes four levers visible: atom number, contrast, interrogation time, and duty factor. It also prevents preparation and readout time from disappearing when two protocols are compared.

For averaging time τ≫Tc\tau\gg T_c, the corresponding atom-projection-noise benchmark for fractional frequency is

σyQPN(τ)≃1ω0CTNTcτ.\sigma_y^{\mathrm{QPN}}(\tau) \simeq \frac{1}{\omega_0CT\sqrt N} \sqrt{\frac{T_c}{\tau}}.

The numerical prefactor depends on the modulation, line shape, estimator, and definition of one error sample. This is an independent-atom benchmark under a local, correctly locked model. It is not automatically the instability of a running clock.

The high carrier frequency of an optical transition improves fractional frequency sensitivity through the factor 1/ω01/\omega_0. It does not by itself remove laser noise, systematic shifts, dead time, or transfer uncertainty.

Successive clock cycles are generally not independent. Oscillator frequency noise has memory, the servo feeds previous outcomes into future controls, and slow systematic variables drift. A state-space model makes these dependencies explicit. Let xjx_j contain the oscillator offset, drift, and selected nuisance parameters; let aja_j denote the known interrogation settings. After observing KjK_j, the controller chooses the correction uju_j for the next transition:

Kj∼p(Kj∣xj,aj),xj+1=f(xj,uj)+wj.K_j\sim p(K_j|x_j,a_j),\qquad x_{j+1}=f(x_j,u_j)+w_j.

Write πj−(x)\pi_j^-(x) for the prior before measurement jj and πj+(x)\pi_j^+(x) for its posterior. The two operations are

πj−(x)=∫p(x∣x′,uj−1) πj−1+(x′) dx′,πj+(x)∝p(Kj∣x,aj) πj−(x).\begin{aligned} \pi_j^-(x) &=\int p(x|x',u_{j-1})\,\pi_{j-1}^+(x')\,dx',\\ \pi_j^+(x) &\propto p(K_j|x,a_j)\,\pi_j^-(x). \end{aligned}

The first line predicts the current state from the previous posterior. The second updates that same state with the current measurement. The controller then chooses uju_j from πj+\pi_j^+. In a locally linear Gaussian model this becomes a Kalman filter; broad periodic likelihoods can require a circular, grid-based, or particle representation.

A scalar example shows why measurement precision and oscillator quality must be optimized together. Suppose the latent cycle-to-cycle frequency follows a random walk,

xj+1=xj+wj,Var⁡(wj)=q,x_{j+1}=x_j+w_j, \qquad \operatorname{Var}(w_j)=q,

and a locally linear atomic readout is

rj=xj+vj,Var⁡(vj)=R.r_j=x_j+v_j, \qquad \operatorname{Var}(v_j)=R.

If PP is the steady-state posterior variance, prediction gives P+qP+q and measurement update gives

P=R(P+q)P+q+R.P = \frac{R(P+q)}{P+q+R}.

The nonnegative solution is

P=q2+4qR−q2.P = \frac{ \sqrt{q^2+4qR}-q }{2}.

Reducing atomic measurement noise RR helps, but the gain depends on process noise qq. When qq is large, oscillator unpredictability replenishes uncertainty between observations. When qq is very small, the filter can average many weak measurements statistically. The prediction variance before the next observation is P+qP+q, even if the posterior PP is small. A continuously available clock output is affected by this between-measurement uncertainty, not just the uncertainty immediately after an update.

Local Oscillator Noise Is Part of the Task

Section titled “Local Oscillator Noise Is Part of the Task”

The local oscillator is not merely a technical imperfection external to quantum metrology. Its phase is precisely what the atoms are asked to estimate and stabilize. Oscillator noise can

  • broaden the phase prior before each measurement;
  • reduce observed contrast when untracked;
  • drive the state outside the discriminator’s local range;
  • correlate outcomes from different cycles;
  • enter through pulse phases and optical-path delivery;
  • be aliased by dead time; and
  • set the benefit obtainable from lower atomic readout noise.

If an untracked Gaussian phase has variance σLO2(T)\sigma_{\mathrm{LO}}^2(T), its average coherence factor is

CLO(T)=exp⁡ ⁣[−σLO2(T)2].C_{\mathrm{LO}}(T) = \exp\!\left[ -\frac{\sigma_{\mathrm{LO}}^2(T)}{2} \right].

Substituting this factor into a fringe model captures contrast loss but not every consequence of colored oscillator noise. The same noise also determines the phase prior, cycle-to-cycle correlations, and slip probability. A full clock model therefore uses a phase-noise or fractional-frequency-noise spectrum and the actual sensitivity function. Noise Spectra develops spectral conventions; the AMO Atomic Clocks page derives the clock-specific Dick-effect sum.

Preparation and detection create intervals during which the atoms do not observe the oscillator. Periodic sampling mixes local-oscillator noise near harmonics of 1/Tc1/T_c into the clock record: the Dick effect. Increasing NN or squeezing the atomic readout does not suppress that aliased oscillator noise. Indeed, reducing projection noise can reveal a Dick-noise floor that was previously hidden.

Important mitigation strategies have different resource costs:

  • faster preparation and readout raise duty factor;
  • interleaved ensembles can provide nearly continuous sensitivity;
  • a quieter oscillator reduces phase diffusion but may require a larger cryogenic, optical, or vibration-isolated subsystem;
  • synchronous comparison rejects shared oscillator noise but changes the claim from independent stability to differential stability;
  • nondestructive or weak measurements can track phase while adding measurement backaction and control complexity.

Achieving nearly continuous atomic sensitivity can require an extra ensemble and coordinated interrogation. Its additional controls and optical paths affect both practical cost and frequency uncertainty.

A two-outcome Ramsey fringe is periodic. Near a chosen operating point the error signal is approximately linear, but outside its capture interval the same measurement can indicate the wrong branch. For a zero-mean Gaussian predicted phase with standard deviation σϕ\sigma_\phi, the probability of leaving the nominal capture interval ∣ϕ∣<ϕcap|\phi|<\phi_{\mathrm{cap}} is

Pout≃erfc⁡ ⁣(ϕcap2σϕ).P_{\mathrm{out}} \simeq \operatorname{erfc}\!\left( \frac{\phi_{\mathrm{cap}}}{\sqrt2\sigma_\phi} \right).

The actual slip probability also depends on measurement noise, the controller, and recovery logic. Identifying PslipP_{\mathrm{slip}} with this tail probability is a simplified model in which every excursion causes a slip.

Even a small per-cycle probability can matter in a long data set. If there are MM nearly independent opportunities to slip, then

P(at least one slip)=1−(1−Pslip)M≃MPslipP(\text{at least one slip}) = 1-(1-P_{\mathrm{slip}})^M \simeq MP_{\mathrm{slip}}

when MPslip≪1MP_{\mathrm{slip}}\ll1. Without independence, the union bound still gives P(at least one slip)≤MPslipP(\text{at least one slip})\le MP_{\mathrm{slip}} for equal marginal probabilities; the exact product formula need not hold.

Longer interrogation increases local frequency information as T2T^2 but also widens the oscillator phase distribution and narrows the unambiguous frequency range. Multi-ensemble protocols can use short or dual-quadrature interrogations to identify the branch for a longer interrogation. Adaptive protocols can carry a full phase posterior and choose TT or analysis phase from its width. Every auxiliary ensemble and short interrogation counts toward the global resource comparison.

A clock that occasionally makes undetected fringe hops may have an impressive conditional Allan deviation after bad runs are removed. Reliability claims must report the detection rule, removed intervals, false-alarm rate, recovery time, and effect on availability.

If independent atomic coherence decays as

C(T)=e−ΓT,C(T)=e^{-\Gamma T},

then the ideal CSS information rate is

F˙δω(T)=NT2e−2ΓTT+td,\dot F_{\delta\omega}(T) = \frac{NT^2e^{-2\Gamma T}}{T+t_d},

where td=Tc−Tt_d=T_c-T is fixed dead time. The optimal TT solves

2T−2Γ−1T+td=0.\frac{2}{T} - 2\Gamma - \frac{1}{T+t_d} =0.

With zero dead time, T∗=1/(2Γ)T_*=1/(2\Gamma). Positive dead time makes longer interrogations relatively more valuable because each cycle carries fixed overhead. Oscillator phase wraps or non-Markovian noise can impose a shorter optimum than this contrast-only model predicts.

This optimization illustrates a recurring rule: maximize information or task utility per wall-clock resource, not information per successful interrogation in isolation.

A CSS has frequency QFI NT2NT^2; an ideal NN-atom GHZ state has N2T2N^2T^2. The latter also has a phase period reduced by NN, faster decoherence under independent noise, and potentially slower preparation. Heisenberg Scaling derives these generator and range comparisons.

For independent Markovian dephasing with single-atom contrast e−ΓTe^{-\Gamma T} and no overhead, the information rates are

F˙CSS=NTe−2ΓT,F˙GHZ=N2Te−2NΓT.\dot F_{\mathrm{CSS}}=NT e^{-2\Gamma T},\qquad \dot F_{\mathrm{GHZ}}=N^2T e^{-2N\Gamma T}.

Their optimal times are 1/(2Γ)1/(2\Gamma) and 1/(2NΓ)1/(2N\Gamma), respectively, and both attain N/(2eΓ)N/(2e\Gamma). This is a comparison under a specific noise and timing model, not a prohibition on entanglement-enhanced clocks. Other states or noise structures can give different improvements. The derivation is developed in Noise and Decoherence in Metrology.

A spin-squeezed state is often more practical than a GHZ state. Its Wineland parameter

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

already compares noise with signal response. In a locally linear Ramsey measurement, an idealized phase variance is

(Δϕ)2≃ξR2N,(\Delta\phi)^2 \simeq \frac{\xi_R^2}{N},

For a locally Gaussian readout with parameter-independent variance this corresponds to Fϕ=N/ξR2F_\phi=N/\xi_R^2; more generally these first and second moments give a lower bound on the readout FI. Spin Squeezing develops the covariance, entanglement witnesses, preparation, and readout.

For the running clock, compare the phase variance after the actual interrogation, preparation time, failed cycles, oscillator noise, and readout. The worked example below shows explicitly how the contrast of the reference and the longer cycle time change the expected gain.

Two clocks interrogated synchronously with equal sensitivity to a shared local oscillator can reject its phase. Choosing the difference sign so the atomic contribution is ωA−ωB\omega_A-\omega_B, a simplified phase is

dj=(ωA−ωB)T+nA,j−nB,j+ϕlink,j,d_j = (\omega_A-\omega_B)T + n_{A,j}-n_{B,j} + \phi_{\mathrm{link},j},

where the common oscillator term has canceled. This can reveal atomic projection noise or a frequency ratio beneath the free-running oscillator noise. For different carrier frequencies or unequal sensitivity functions, frequency-transfer factors and appropriate weighting are required for this cancellation. It does not directly show how either clock would perform with an independent oscillator.

For two fractional-frequency estimates with covariance, the differential variance is

Var⁡(yA−yB)=Var⁡(yA)+Var⁡(yB)−2Cov⁡(yA,yB).\operatorname{Var}(y_A-y_B) = \operatorname{Var}(y_A) + \operatorname{Var}(y_B) - 2\operatorname{Cov}(y_A,y_B).

Ignoring the covariance can either exaggerate or hide noise. Shared lasers, environmental monitors, atom preparation, transfer links, and data processing all create correlations. Conversely, an independent comparison includes both clocks and the link; attributing the result to one clock requires an additional model or a third reference.

The same distinction applies to entanglement-enhanced comparisons. A differential gain with a common oscillator establishes a valuable network or ratio result under that architecture. A claim about stand-alone timekeeping must include the oscillator and control resources needed at each node.

Define fractional frequency deviation

y(t)=ν(t)−ν0ν0.y(t)=\frac{\nu(t)-\nu_0}{\nu_0}.

For adjacent averages yˉk(τ)\bar y_k(\tau), Allan variance is

σy2(τ)=12E ⁣[(yˉk+1−yˉk)2].\sigma_y^2(\tau) = \frac12 \mathbb E\!\left[ (\bar y_{k+1}-\bar y_k)^2 \right].

It is a stability statistic for a specified record and averaging time. It is not automatically a frequentist confidence interval for the mean, a Bayesian posterior width, or a systematic uncertainty. Drift, flicker floors, gaps, servo transients, and selection can all invalidate a casual 1/τ1/\sqrt\tau extrapolation.

Systematic accuracy is a separate estimation problem. A schematic clock measurement equation is

ycorr=ymeas−∑rβrxr,y_{\mathrm{corr}} = y_{\mathrm{meas}} - \sum_r \beta_r x_r,

where xrx_r are environmental or operating variables and βr\beta_r are sensitivities. Uncertainty in both, together with covariance, propagates to the corrected result. Quantum Fisher information for the Ramsey phase does not bound an unmodeled bias. Detailed shift evaluation belongs to the AMO clock pages.

A mature result therefore keeps at least four objects separate:

  • single-cycle phase resolution;
  • locked-clock instability versus averaging time;
  • systematic uncertainty of the realized frequency;
  • task loss, such as time error, ratio uncertainty, availability, or anomaly-detection probability.

Optimizing one does not guarantee improvement in the others.

Worked comparison with reduced contrast and longer cycles

Section titled “Worked comparison with reduced contrast and longer cycles”

Consider an optical clock with

ν0=4.3×1014 Hz,N=104,T=0.50 s,\nu_0=4.3\times10^{14}\,\mathrm{Hz}, \quad N=10^4, \quad T=0.50\,\mathrm{s},

C=0.80C=0.80, and Tc=1.0 sT_c=1.0\,\mathrm{s}. The white-frequency-noise model has the one-second coefficient

σyQPN(1 s)≃12π(4.3×1014)(0.80)(0.50)(100)≃9.3×10−18.\begin{aligned} \sigma_y^{\mathrm{QPN}}(1\,\mathrm{s}) &\simeq \frac{1}{ 2\pi(4.3\times10^{14})(0.80)(0.50)(100) } \\ &\simeq 9.3\times10^{-18}. \end{aligned}

Suppose a squeezed protocol has metrological parameter ξR2=10−5/10≃0.316\xi_R^2=10^{-5/10}\simeq0.316 but increases cycle time to 1.20 s1.20\,\mathrm{s}. If all other clock noise is absent and ξR2\xi_R^2 already includes the response reduction, its phase variance is ξR2/N\xi_R^2/N. The actual CSS reference has phase variance 1/(NC2)1/(NC^2), so for averaging times long compared with both cycles the instability ratio is

σysqσyCSS=CξR21.201.00≃0.493.\frac{\sigma_y^{\mathrm{sq}}}{\sigma_y^{\mathrm{CSS}}} = C\sqrt{\xi_R^2} \sqrt{\frac{1.20}{1.00}} \simeq 0.493.

The idealized improvement relative to this contrast-0.800.80 reference is about 1/0.493≃2.031/0.493\simeq2.03. The 55 dB Wineland value was defined relative to a unit-contrast coherent spin, so it is not itself the variance ratio to the degraded reference used here. If an experiment instead reports a variance ratio of 0.3160.316 directly relative to its actual CSS protocol, the cycle-time penalty would give 0.316×1.20≃0.616\sqrt{0.316\times1.20}\simeq0.616. State which reference the reported gain uses. If Dick noise or oscillator phase slips already exceed the CSS projection-noise term, the total improvement is smaller and may vanish.

For NN two-level atoms interrogated for time TT, calculate the ideal frequency QFI of a CSS and a GHZ state. What additional issue appears in the GHZ likelihood?

Solution

Frequency is encoded by e−iδωTJze^{-i\delta\omega TJ_z}, so

Fδω=4T2Var⁡(Jz).F_{\delta\omega} = 4T^2\operatorname{Var}(J_z).

For a CSS, Var⁡(Jz)=N/4\operatorname{Var}(J_z)=N/4, giving

FδωCSS=NT2.F_{\delta\omega}^{\mathrm{CSS}}=NT^2.

For a GHZ state, Var⁡(Jz)=N2/4\operatorname{Var}(J_z)=N^2/4, giving

FδωGHZ=N2T2.F_{\delta\omega}^{\mathrm{GHZ}}=N^2T^2.

The GHZ signal depends on NδωTN\delta\omega T, so its phase period is reduced by a factor NN. A single sine readout also has a reflection ambiguity within that period. The local QFI does not resolve those branches.

A Ramsey clock has N=2500N=2500, C=0.75C=0.75, T=0.20 sT=0.20\,\mathrm{s}, Tc=0.50 sT_c=0.50\,\mathrm{s}, and ν0=9.192631770 GHz\nu_0=9.192631770\,\mathrm{GHz}. Estimate its QPN-limited Allan deviation at τ=100 s\tau=100\,\mathrm{s}.

Solution

Use

σyQPN(τ)=12πν0CTNTcτ.\sigma_y^{\mathrm{QPN}}(\tau) = \frac{1}{2\pi\nu_0CT\sqrt N} \sqrt{\frac{T_c}{\tau}}.

Substitution gives

σyQPN(100 s)=0.50/1002π(9.192631770×109)(0.75)(0.20)(50)≃1.63×10−13.\begin{aligned} \sigma_y^{\mathrm{QPN}}(100\,\mathrm{s}) &= \frac{ \sqrt{0.50/100} }{ 2\pi(9.192631770\times10^9)(0.75)(0.20)(50) } \\ &\simeq 1.63\times10^{-13}. \end{aligned}

This is a projection-noise benchmark. It omits oscillator noise, Dick aliasing, detection noise, shifts, and servo dynamics.

Assume zero dead time and C(T)=e−ΓTC(T)=e^{-\Gamma T}. Maximize the CSS frequency information rate and find its maximum.

Solution

With Tc=TT_c=T,

F˙(T)=NTe−2ΓT.\dot F(T)=NTe^{-2\Gamma T}.

Differentiating,

dF˙dT=Ne−2ΓT(1−2ΓT).\frac{d\dot F}{dT} = Ne^{-2\Gamma T}(1-2\Gamma T).

Thus

T∗=12Γ,T_*=\frac{1}{2\Gamma},

and

F˙(T∗)=N2eΓ.\dot F(T_*) = \frac{N}{2e\Gamma}.

The result assumes independent Markovian dephasing and no phase-wrap or oscillator constraint.

For Γ=1 s−1\Gamma=1\,\mathrm{s}^{-1} and fixed dead time td=0.20 st_d=0.20\,\mathrm{s}, solve the interrogation-time condition

2T−2Γ−1T+td=0.\frac2T-2\Gamma-\frac1{T+t_d}=0.
Solution

Multiplying by T(T+td)T(T+t_d) gives

2(T+td)−2ΓT(T+td)−T=0.2(T+t_d)-2\Gamma T(T+t_d)-T=0.

With the stated values,

2T2−0.6T−0.4=0.2T^2-0.6T-0.4=0.

The positive root is

T∗=0.6+0.36+3.24≃0.622 s.T_* = \frac{0.6+\sqrt{0.36+3.2}}{4} \simeq 0.622\,\mathrm{s}.

This exceeds the zero-dead-time optimum 0.5 s0.5\,\mathrm{s} because a longer interrogation amortizes the fixed overhead.

For the scalar random-walk clock model, let process variance be q=4×10−4q=4\times10^{-4} and atomic measurement variance be R=9×10−4R=9\times10^{-4}. Find the steady-state posterior variance PP and standard deviation.

Solution

Use

P=q2+4qR−q2.P = \frac{\sqrt{q^2+4qR}-q}{2}.

Then

P=(4×10−4)2+4(4×10−4)(9×10−4)−4×10−42≃4.32×10−4.\begin{aligned} P &= \frac{ \sqrt{(4\times10^{-4})^2 +4(4\times10^{-4})(9\times10^{-4})} -4\times10^{-4} }{2} \\ &\simeq 4.32\times10^{-4}. \end{aligned}

Therefore

P≃2.08×10−2.\sqrt P\simeq2.08\times10^{-2}.

The posterior variance is neither qq nor RR; it is set by their dynamical balance.

A clock has Gaussian predicted phase with σϕ=0.25 rad\sigma_\phi=0.25\,\mathrm{rad} and capture half-width ϕcap=π/2\phi_{\mathrm{cap}}=\pi/2. Estimate the outside-capture probability. Under the additional approximation that each excursion causes a slip, find the probability of at least one slip in 10910^9 independent cycles.

Solution

The Gaussian outside-capture probability is

Pslip≃erfc⁡ ⁣(π/22(0.25))=erfc⁡(4.44).P_{\mathrm{slip}} \simeq \operatorname{erfc}\!\left( \frac{\pi/2}{\sqrt2(0.25)} \right) = \operatorname{erfc}(4.44).

Numerically this is approximately

Pslip≃3.32×10−10P_{\mathrm{slip}} \simeq 3.32\times10^{-10}

per independent opportunity. Over 10910^9 cycles, the small-probability estimate gives an expected slip count of about 0.3320.332 and probability 1−e−0.332≃0.2821-e^{-0.332}\simeq0.282 of at least one slip. Very small per-cycle risks can therefore matter in long operation.

Two clocks have individual fractional-frequency variances 99 and 1616 in arbitrary units and covariance 1010 because they share a local oscillator. Find the variance of their difference. What value would be inferred if the covariance were ignored?

Solution

The differential variance is

Var⁡(yA−yB)=9+16−2(10)=5.\operatorname{Var}(y_A-y_B) = 9+16-2(10) = 5.

Ignoring covariance would give 2525, five times too large. The shared oscillator can be strongly rejected in the difference. The low differential variance does not imply that either stand-alone output has variance 55.

8. Why Allan variance does not measure a constant bias

Section titled “8. Why Allan variance does not measure a constant bias”

For fractional frequency y(t)=b+aty(t)=b+at, compute the Allan variance using adjacent intervals of duration τ\tau. What happens for a constant offset?

Solution

The interval average is yˉk=b+a(k+12)τ\bar y_k=b+a(k+\tfrac12)\tau. Adjacent averages differ by aτa\tau, giving

σy2(τ)=a2τ22.\sigma_y^2(\tau)=\frac{a^2\tau^2}{2}.

For a=0a=0, the Allan variance is zero even when the constant offset bb is nonzero. A clock can be stable while systematically shifted. Conversely, linear drift produces Allan deviation proportional to τ\tau, so extending an independent-white-noise τ−1/2\tau^{-1/2} law would give the wrong behavior.

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