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

Einstein Equivalence Principle (EEP)

Author: Tianjiang Says

Reference: Li Y et al. 2026 Chin. Phys. Lett. 43 031101, Will C M 2014 Living Rev. Relativ. 17 4

Website: https://cislunarspace.cn

Definition

The Einstein Equivalence Principle (EEP) is the cornerstone of general relativity and the key framework for testing GR's validity. EEP states: within any freely-falling local reference frame in any gravitational field, the laws of non-gravitational physics have exactly the same form as in the absence of gravity.

EEP contains three sub-principles, each constraining the gravitational invariance of physical laws from different perspectives.

Three Sub-Principles

Weak Equivalence Principle (WEP)

The Weak Equivalence Principle is the most classical statement of equivalence, also known as "inertial mass equals gravitational mass":

All objects accelerate identically in a gravitational field, independent of their composition and structure.

Mathematically: mimg=1\frac{m_i}{m_g} = 1mg​mi​​=1

WEP verification experiments include:

  • Free fall experiments since Newton's era
  • Eötvös torsion balance experiments
  • MICROSCOPE satellite (precision reaching 10−1510^{-15}10−15)

Local Lorentz Invariance (LLI)

Local Lorentz Invariance states:

In the local inertial frame at any spacetime point, the expressions of all non-gravitational physical laws are independent of the reference frame's velocity.

LLI verification typically involves comparing oscillator frequencies of atomic clocks with different spin orientations.

Local Position Invariance (LPI)

Local Position Invariance is the sub-principle most directly related to gravitational redshift:

In a freely-falling local reference frame, the results of any non-gravitational experiment are independent of when and where in spacetime the experiment is performed.

The core meaning of LPI is that fundamental physical constants (such as fine structure constant α\alphaα, electron-proton mass ratio me/mpm_e/m_pme​/mp​, etc.) do not depend on gravitational potential. Gravitational redshift experiments test this assumption by constraining LPI.

Mathematical Formulation of LPI

The relationship between gravitational redshift and LPI is described by introducing a violation parameter α\alphaα:

Δff=(1+α)ΔUc2\frac{\Delta f}{f} = (1 + \alpha) \frac{\Delta U}{c^2} fΔf​=(1+α)c2ΔU​

Where:

  • Δf/f\Delta f/fΔf/f is the relative frequency shift between two clocks
  • ΔU\Delta UΔU is the gravitational potential difference
  • ccc is the speed of light
  • α\alphaα is the LPI violation parameter

If LPI holds, then α=0\alpha = 0α=0; if LPI is violated, α\alphaα deviates from zero.

Testing Status of Sub-Principles

Sub-PrincipleTesting PrecisionRepresentative Experiment
WEP10−1510^{-15}10−15MICROSCOPE satellite
LLI10−2210^{-22}10−22Atomic clock comparison
LPI10−510^{-5}10−5Galileo satellite gravitational redshift

Currently, LPI is the least rigorously tested sub-principle of EEP, which is why gravitational redshift experiments continue to receive attention.

Relation to Gravitational Redshift Measurements

Gravitational redshift experiments are the primary means of testing LPI. By measuring the frequency difference between clocks at different gravitational potentials, one can constrain the LPI violation parameter α\alphaα.

Historically significant gravitational redshift experiments:

  1. Pound-Rebka-Snider (1960s): Ground experiment, precision ~1%
  2. Gravity Probe A (1976): Space maser clock, precision 1.41×10−41.41 \times 10^{-4}1.41×10−4
  3. Galileo Satellites (2018): Elliptical orbit modulation, precision 0.19×10−50.19 \times 10^{-5}0.19×10−5
  4. DRO-A Satellite (2025): First cislunar DRO measurement, precision 8.74×10−38.74 \times 10^{-3}8.74×10−3

Future Prospects for Cislunar Measurements

The unique environment of cislunar space provides new opportunities for LPI testing:

  1. Larger gravitational potential difference: DRO gravitational potential difference (∼6.8×10−10\sim 6.8 \times 10^{-10}∼6.8×10−10) is orders of magnitude larger than ground experiments
  2. Longer observation time: DRO orbits are stable, enabling long-term continuous observation
  3. Higher precision atomic clocks: With clocks achieving 10−1610^{-16}10−16 accuracy, precision could reach 10−610^{-6}10−6

Related Concepts

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

References

  • Will C M 2014 Living Rev. Relativ. 17 4
  • Li Y, Liu T et al. 2026 Chin. Phys. Lett. 43 031101
  • Delva P et al. 2018 Phys. Rev. Lett. 121 231101
  • Herrmann S et al. 2018 Phys. Rev. Lett. 121 231102
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