Cislunar Space Beginner's GuideCislunar Space Beginner's Guide
Satellite Orbit Simulation
Cislunar Glossary
Resources & Tools
Blue Team Research
Space News
AI Q&A
Forum
Home
Gitee
GitHub
  • 简体中文
  • English
Satellite Orbit Simulation
Cislunar Glossary
Resources & Tools
Blue Team Research
Space News
AI Q&A
Forum
Home
Gitee
GitHub
  • 简体中文
  • English
  • Site map

    • Home (overview)
    • Intro · what is cislunar space
    • Orbits · spacecraft trajectories
    • Frontiers · directions & labs
    • Glossary · terms & definitions
    • Tools · data & code
    • News · space industry archive
    • Topic · blue-team research
  • Cislunar glossary (terms & definitions)

    • Cislunar Space Glossary
    • Dynamics models

      • Circular Restricted Three-Body Problem (CR3BP)
      • CR3BP with Low-Thrust (CR3BP-LT)
      • A2PPO (Attention-Augmented Proximal Policy Optimization)
      • Curriculum Learning
      • Low-Thrust Transfer MDP Formulation
      • Generalized Advantage Estimation (GAE)
      • Direct Collocation
      • Birkhoff-Gustavson Normal Form
      • Central Manifold
      • Action-Angle Variables
      • Poincaré Section
      • Clohessy-Wiltshire (CW) Equation
      • Patched Method (拼接法)
      • Continuation (延拓)
      • Differential Correction (微分修正)
      • Poincaré Map (庞加莱图)
      • Impulsive Maneuver (脉冲机动)
      • Zero-Velocity Surface
      • Hill Three-Body Problem
      • Bicircular Four-Body Problem
      • Quasi-Bicircular Four-Body Problem
      • Strobe Map
      • Stability Set
      • Backward Stability Set
      • Capture Set
      • /en/glossary/dynamics/batch-deployment.html
      • /en/glossary/dynamics/state-dependent-tsp.html
      • /en/glossary/dynamics/q-law.html
      • /en/glossary/dynamics/mass-discontinuity.html
      • /en/glossary/dynamics/equinoctial-elements.html
      • /en/glossary/dynamics/dynamic-programming.html
      • /en/glossary/dynamics/coasting-arc.html
    • Mission orbits

      • Distant Retrograde Orbit (DRO)
      • Near-Rectilinear Halo Orbit (NRHO)
      • Earth-Moon L1/L2 Halo Orbit (EML1/EML2 Halo)
      • DRO Constellation
      • Orbit Identification
      • Transfer Orbit (转移轨道)
      • Perilune (近月点)
      • Apolune (远月点)
      • Retrograde (逆行)
      • Prograde (顺行)
      • Parking Orbit (停泊轨道)
      • Free-Return Trajectory (自由返回轨道)
      • Halo Orbit (Halo 轨道)
      • Lissajous Orbit (Lissajous 轨道)
      • Lyapunov Orbit (Lyapunov 轨道)
      • Cycler Trajectory
      • Multi-Revolution Halo Orbit
      • Ballistic Capture Orbit
      • Low-Energy Transfer Orbit
      • Full Lunar Surface Coverage Orbit
      • /en/glossary/orbits/hub-and-spoke.html
    • Navigation

      • X-ray Pulsar Navigation
      • LiAISON Navigation
    • Lunar minerals

      • Changeite-Mg (Magnesium Changeite)
      • Changeite-Ce (Cerium Changeite)
    • Other

      • Starshade
      • Noncooperative Target
      • Spacecraft Intention Recognition
      • Chain-of-Thought (CoT) Prompting
      • Low-Rank Adaptation (LoRA)
      • Prompt Tuning (P-tuning)
      • Cislunar Space (地月空间)
      • Low Earth Orbit / LEO (低地球轨道)
      • Lunar Gravity Assist / LGA (月球借力)
      • Powered Lunar Flyby / PLF (有动力月球借力)
      • Weak Stability Boundary / WSB (弱稳定边界)
      • /en/glossary/other/libration-point.html
      • Orbit Insertion (入轨)
      • /en/glossary/other/orbital-residence-platform.html
    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • General Dynamics Mission Systems
      • GITAI USA
      • Lockheed Martin
      • Northrop Grumman
      • Quindar
      • Raytheon Missiles & Defense
      • Sci-Tec
      • SpaceX
      • True Anomaly
      • Turion Space
    • Military space doctrine

      • Space Superiority
      • Competitive Endurance
      • DOTMLPF-P Framework
      • Mission Command
      • Force Design
      • Force Development
      • Force Generation
      • Force Employment
      • Space Force Generation Process (SPAFORGEN)
      • Mission Delta (MD)
      • System Delta (SYD)
      • Space Mission Task Force (SMTF)
      • Commander, Space Forces (COMSPACEFOR)
      • Component Field Commands
      • Space Domain Awareness (SDA)
      • Counterspace Operations
      • Resilient/Disaggregated Architecture
      • Operational Test and Training Infrastructure (OTTI)
      • Golden Dome
    • Observation techniques

      • Image Stacking
      • Shift-and-Add (SAA)
      • Synthetic Tracking
      • Sidereal Tracking
      • Signal-to-Noise Ratio (SNR)
      • Astrometry
      • Source Extraction
      • Ephemeris Correlation
      • Cislunar Moving Objects
      • Lunar Glare Zone
      • Image Registration
      • Background Star Elimination
      • Segmentation Map
      • Hot Pixel
    • Satellite Communication & TT&C

      • BeiDou Satellite System
      • Inter-Satellite Link (ISL)
      • All-Time Seamless Communication
      • Constellation Networking
      • Microwave Link
      • Laser-Microwave Communication

Allan Deviation (ADEV)

Author: Tianjiang Says

Reference: Li Y et al. 2026 Chin. Phys. Lett. 43 031101

Website: https://cislunarspace.cn

Definition

Allan Deviation (ADEV) is a statistical measure for evaluating frequency source stability, proposed by David W. Allan in 1966. Unlike traditional standard deviation, ADEV can distinguish different types of noise processes (such as white noise, flicker noise, random walk noise, etc.) and avoids divergence issues when noise is non-stationary.

ADEV is the core metric for evaluating atomic clock and oscillator performance in time-frequency metrology.

Mathematical Definition

For adjacent frequency measurements yˉi\bar{y}_iyˉ​i​ at sampling interval τ\tauτ, ADEV is defined as:

σy2(τ)=12(N−1)∑i=1N−1(yˉi+1−yˉi)2\sigma_y^2(\tau) = \frac{1}{2(N-1)} \sum_{i=1}^{N-1} (\bar{y}_{i+1} - \bar{y}_i)^2 σy2​(τ)=2(N−1)1​i=1∑N−1​(yˉ​i+1​−yˉ​i​)2

Where NNN is the number of samples and yˉi\bar{y}_iyˉ​i​ is the average relative frequency offset during the iii-th averaging time τ\tauτ.

The corresponding Allan deviation is:

ADEV=σy(τ)=σy2(τ)\text{ADEV} = \sigma_y(\tau) = \sqrt{\sigma_y^2(\tau)} ADEV=σy​(τ)=σy2​(τ)​

Difference from Standard Deviation

Traditional standard deviation (StdDev) has limitations when evaluating frequency stability: when noise type is flicker frequency noise, standard deviation diverges with increasing sample size—meaning infinite samples still cannot achieve convergence.

ADEV advantages:

  • Converges for multiple noise types
  • Can identify noise power law types
  • Has clear correspondence with physical processes
Noise TypeStdDev BehaviorADEV Behavior
White phase noiseDivergesConverges ∝τ−1\propto \tau^{-1}∝τ−1
Flicker phase noiseDivergesConverges ∝τ0\propto \tau^{0}∝τ0
White frequency noiseConvergesConverges ∝τ−1/2\propto \tau^{-1/2}∝τ−1/2
Flicker frequency noiseDivergesConverges ∝τ0\propto \tau^{0}∝τ0
Random walk frequency noiseConvergesConverges ∝τ1/2\propto \tau^{1/2}∝τ1/2

Modified Allan Deviation (MDEV)

The Modified Allan Deviation (MDEV) used in DRO-A gravitational redshift experiments:

MDEV=12(N−2τ0)∑i=1N−2(1τ2∫τ0τ0+τ∫τ0τ0+τx˙(t2)−x˙(t1) dt1 dt2)2\text{MDEV} = \sqrt{\frac{1}{2(N-2\tau_0)} \sum_{i=1}^{N-2} \left( \frac{1}{\tau^2} \int_{\tau_0}^{\tau_0+\tau} \int_{\tau_0}^{\tau_0+\tau} \dot{x}(t_2) - \dot{x}(t_1) \, dt_1 \, dt_2 \right)^2} MDEV=2(N−2τ0​)1​i=1∑N−2​(τ21​∫τ0​τ0​+τ​∫τ0​τ0​+τ​x˙(t2​)−x˙(t1​)dt1​dt2​)2​

MDEV advantages over ADEV:

  • Better confidence for the same noise type
  • Can distinguish white frequency noise from flicker frequency noise

Typical Performance Specifications

Typical ADEV values for different atomic clock types:

Oscillator Typeτ=1\tau = 1τ=1 sτ=1000\tau = 1000τ=1000 sτ=10000\tau = 10000τ=10000 s
Passive Hydrogen Maser (PHM)10−1210^{-12}10−1210−1410^{-14}10−1410−1410^{-14}10−14
Cesium Beam Tube10−1110^{-11}10−1110−1310^{-13}10−1310−1310^{-13}10−13
Rubidium10−1110^{-11}10−1110−1210^{-12}10−1210−1210^{-12}10−12
Strontium Optical Lattice Clock10−1610^{-16}10−1610−1810^{-18}10−1810−1810^{-18}10−18

Application in DRO-A Experiment

The DRO-A satellite gravitational redshift experiment measured satellite-ground time-frequency comparison stability:

Averaging TimeApril 28 MDEVApril 29 MDEV
10 s6.14×10−136.14 \times 10^{-13}6.14×10−137.01×10−137.01 \times 10^{-13}7.01×10−13
100 s8.03×10−138.03 \times 10^{-13}8.03×10−138.03×10−138.03 \times 10^{-13}8.03×10−13
1000 s4.58×10−144.58 \times 10^{-14}4.58×10−146.98×10−146.98 \times 10^{-14}6.98×10−14
2000 s1.27×10−141.27 \times 10^{-14}1.27×10−142.10×10−142.10 \times 10^{-14}2.10×10−14

Key findings:

  • Stability at 1000s averaging exceeds 7×10−147 \times 10^{-14}7×10−14
  • Stability at 2000s averaging exceeds 2×10−142 \times 10^{-14}2×10−14
  • Stability outperforms accuracy by two orders of magnitude, meaning stability is the primary limiting factor for gravitational redshift measurements

Related Concepts

  • Passive Hydrogen Maser (PHM)
  • Gravitational Redshift
  • Dual One-Way Ranging (DOWR)
  • Distant Retrograde Orbit (DRO)

References

  • Allan D W 1966 Proc. IEEE 54 221
  • Li Y, Liu T et al. 2026 Chin. Phys. Lett. 43 031101
Improve this page
Last Updated: 4/29/26, 4:41 PM
Contributors: Cron Job
地月空间入门指南
Cislunar Space Beginner's GuideYour guide to cislunar space
View on GitHub

Navigate

  • Home
  • About
  • Space News
  • Glossary

Content

  • Cislunar Orbits
  • Research
  • Resources
  • Blue Team

English

  • Home
  • About
  • Space News
  • Glossary

Follow Us

© 2026 Cislunar Space Beginner's Guide  |  湘ICP备2026006405号-1
Related:智慧学习助手 UStudy航天任务工具箱 ATK
支持我
鼓励和赞赏我感谢您的支持