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    • Home (overview)
    • What is cislunar space
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    • Glossary · terms & definitions
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  • Cislunar glossary (terms & definitions)

    • Cislunar Space Glossary
    • Fundamentals

      • Absolute Range
      • Aerodynamic Coefficient
      • Aerodynamic Moment
      • Aerospace Vehicle
      • Allan Deviation (ADEV)
      • Ballistic Coefficient
      • Bi-Elliptic Transfer
      • Body Frame
      • Celestial Coordinate System
      • Celestial Sphere
      • Characteristic Velocity
      • Coverage Angle
      • Dual One-Way Ranging (DOWR)
      • Earth Ellipsoid
      • Earth Oblateness Perturbation
      • Earth-Centered Earth-Fixed Frame (ECEF)
      • Einstein Equivalence Principle (EEP)
      • Energy Parameter
      • Earth Observation (EO)
      • Finite Thrust Maneuver
      • Free-Flight Phase
      • Free-Flight Trajectory
      • Frozen Orbit
      • Gaussian Perturbation Equations
      • Geocentric Inertial Frame
      • GPS Time
      • Gravitational Potential
      • Gravitational Redshift
      • Gravity Turn
      • Gravity vs Gravitation
      • High Altitude Airship (HAA)
      • Hit Equation
      • Hohmann Transfer
      • Inertial Navigation System
      • Instantaneous Balance Assumption
      • In-Situ Resource Utilization (ISRU)
      • Julian Date
      • Kepler's Equation
      • Korea Multi-Purpose Satellite (KOMPSAT)
      • Lagrangian Perturbation Equations
      • Launch Azimuth
      • Launch Window
      • Lift-to-Drag Ratio
      • Load Factor
      • Longitudinal and Lateral Motion
      • Lunar Lander
      • Minimum Energy Trajectory
      • Near-space
      • Newton's Iteration Method
      • Nuri (KSLV-II)
      • Nutation
      • Optimal Velocity Inclination
      • Orbit Capture
      • Orbit Insertion Conditions
      • Orbital Elements
      • Orbital Equation
      • Orbital Maneuver
      • Orbital Phase
      • Orbital Transfer Vehicle
      • Passive Hydrogen Maser (PHM)
      • Perturbation Motion
      • Phasing Orbit
      • Pitch Program Angle
      • Powered Phase
      • Precession
      • Center of Pressure
      • Range Error Coefficient
      • Reentry Corridor
      • Reentry Phase
      • Repeat Ground Track Orbit
      • Reusable Launch Vehicle
      • Synthetic Aperture Radar (SAR)
      • Satellite Ring
      • Sequential Quadratic Programming
      • Skip Reentry
      • Solar Exposure Factor
      • Specific Angular Momentum
      • Specific Impulse
      • Stagnation Heat Flux
      • Standard Atmosphere
      • Stratospheric Airship
      • Subsatellite Track
      • Sun-Synchronous Orbit
      • Thrust-to-Weight Ratio
      • Thrust
      • Total Angle of Attack
      • Trajectory Equation
      • Trajectory Optimization
      • Trim Angle of Attack
      • True Anomaly
      • Tsiolkovsky Rocket Equation
      • Powered Phase Turning Process
      • Two-Body Problem
      • Coordinated Universal Time
      • Variation of Parameters
      • Velocity Frame
      • Velocity Inclination Angle
      • Vis-Viva Equation
      • Very Low Earth Orbit (VLEO)
      • Walker Constellation
      • Zero-Angle-of-Attack Reentry
    • Dynamics & math

      • A* Search Algorithm (A* Search)
      • A2PPO (Attention-Augmented Proximal Policy Optimization)
      • Action-Angle Variables
      • Backstepping Sliding Mode Control
      • Backward Stability Set
      • Bang-bang Control (Bang-bang Control)
      • Barycentric Synodic Coordinate System
      • Batch Deployment (Batch Deployment)
      • Bicircular Four-Body Problem
      • Birkhoff-Gustavson Normal Form
      • Buoyancy-weight Imbalance
      • Capture Set
      • Central Manifold
      • Chaos Effect
      • Clohessy-Wiltshire (CW) Equation
      • Co-state Normalization (Co-state Normalization)
      • Co-state Variables
      • Coasting Arc (Coasting Arc)
      • Continuation Method (Parameter Continuation)
      • Continuation
      • Cooperative Agent (CA)
      • CR3BP with Low-Thrust (CR3BP-LT)
      • Circular Restricted Three-Body Problem (CR3BP)
      • Curriculum Learning
      • Deep Deterministic Policy Gradient (DDPG)
      • Deep Reinforcement Learning
      • Detection Graph
      • Differential Correction
      • Differential Evolution (DE) Algorithm
      • Differential Games (Differential Games)
      • Direct Collocation
      • Dynamic Programming (Dynamic Programming)
      • Dynamic Target Method
      • Ephemeris Model
      • Equinoctial Orbital Elements (Equinoctial Orbital Elements)
      • Earth Restricted Three-Body Problem (ERTBP)
      • Fuel-optimal Control
      • Fuzzy Backstepping Control
      • Generalized Advantage Estimation (GAE)
      • Gaussian Process Regression
      • Geocentric Rotating Coordinate System (GRC)
      • Hamiltonian
      • Hybrid Cluster Particle Swarm Optimization (HCPSO)
      • Heteroclinic Orbit Transfer (Heteroclinic Orbit Transfer)
      • Hill Three-Body Problem
      • Homotopy Method (Homotopy Method)
      • Improved Baseline Control-Point Method (Improved Baseline Control-Point Method)
      • Impulsive Maneuver
      • Initial Value Optimization
      • Invariant Manifold (Invariant Manifold)
      • J2000 Geocentric Equatorial Coordinate System (J2000 Geocentric Equatorial Coordinate System)
      • Jacobi Constant (Jacobi Integral)
      • K-Means Clustering (K-Means Clustering)
      • K-Medoids Clustering (K-Medoids Clustering)
      • KD-Tree (KD-Tree)
      • Libration Point (Equilibrium Point)
      • Libration Point Spacecraft Body Coordinate System (Libration Point Spacecraft Body Coordinate System)
      • Libration Point Spacecraft Orbital Coordinate System (Libration Point Spacecraft Orbital Coordinate System)
      • Lindstedt-Poincare Method (Lindstedt-Poincare Method)
      • L2-centered Rotating Coordinate System (L2-centered Rotating Coordinate System, LRC)
      • LSTM Neural Network
      • Low-Thrust Transfer MDP Formulation
      • Mass Discontinuity (Mass Discontinuity)
      • Multi-Objective Monte Carlo Tree Search (MO-MCTS)
      • Modal Analysis
      • Monodromy Matrix
      • Monte Carlo Tree Search
      • Newton-Euler Equations
      • NSGA II (Non-dominated Sorting Genetic Algorithm II)
      • Pareto Optimality
      • Particle Swarm Optimization
      • Patch Point (Splicing Point)
      • Patched Method
      • Poincaré Map
      • Poincaré Section
      • Pontryagin's Maximum Principle
      • Pseudo-Arclength Continuation
      • Spacecraft Pursuit-Evasion Game
      • Q-Law Control Law
      • Quasi-Bicircular Problem (QBCP)
      • Quasi-Bicircular Four-Body Problem
      • Reachable Set
      • Reduced-Order Dynamic Equations
      • Regional Station-keeping Control
      • Regularization
      • Reinforcement Learning Enhanced Particle Swarm Optimization (RLEPSO)
      • Saddle-Point Strategy
      • Seven-node Model
      • Shooting Method
      • Six-DOF Motion Equations
      • Sliding Mode Control
      • Solar Radiation Pressure (SRP)
      • Stability Index
      • Stability Set
      • State-Dependent Traveling Salesman Problem (SDTSP)
      • State Transition Matrix (STM)
      • Static Lift
      • Strobe Map
      • Switching Function
      • Targeting Method
      • Thermo-mechanical Coupling Model
      • Thermodynamic Model
      • Two-Point Boundary Value Problem (TPBVP)
      • Trim Condition
      • Two-Dominant Invariant Manifold Method
      • Two-Level Differential Correction Method
      • Two-node Model
      • Variational Mode Decomposition
      • Zero-Effort Miss (ZEM)
      • Zero-Velocity Surface
    • Mission orbits

      • Apolune
      • Axial Orbit
      • Ballistic Capture Orbit
      • Butterfly Orbit
      • Cycler Trajectory
      • Distant Prograde Orbit (DPO)
      • DRO Constellation
      • Distant Retrograde Orbit (DRO)
      • Earth-Moon L1/L2 Halo Orbit (EML1/EML2 Halo)
      • Free-Return Trajectory
      • Full Lunar Surface Coverage Orbit
      • Halo Orbit
      • Heteroclinic Connection
      • Horseshoe Orbit
      • Hub-and-Spoke
      • Lissajous Orbit
      • Long Period Orbit
      • Low Prograde Orbit (LoPO)
      • Low-Energy Transfer Orbit
      • Low-Thrust Transfer Orbit
      • Lyapunov Orbit
      • Multi-Revolution Halo Orbit
      • Near-Rectilinear Halo Orbit (NRHO)
      • Orbit Identification
      • Orbit Keeping (Station-Keeping)
      • Parking Orbit
      • Perilune
      • Polynomial Constraint Station-Keeping
      • Primary Impulse Orbit Transfer
      • Prograde
      • Quasi-Periodic Orbit
      • Resonance Orbit
      • Retrograde
      • Short Period Orbit
      • Transfer Orbit
      • Triangular Libration Points
      • Vertical Orbit
    • Navigation & systems

      • Altitude Regulation
      • Autonomous Navigation
      • Cislunar Spatiotemporal Reference
      • Earth-Moon Hybrid Navigation
      • Extended Kalman Filter (EKF)
      • GPS Aided GEO Augmented Navigation (GAGAN)
      • Earth GNSS Weak Signal Navigation
      • Inter-Satellite Link Navigation
      • Indian Regional Navigation Satellite System (IRNSS)
      • LEO Navigation Augmentation
      • LiAISON Navigation
      • LunaNet (Lunar Network)
      • Lunar Navigation Constellation
      • Moonlight Initiative
      • Observability
      • Positioning, Navigation, and Timing (PNT)
      • Sun-Earth-Moon Autonomous Navigation
      • Tiandu-1
      • Trajectory Planning
      • X-ray Pulsar Navigation
    • Astronomy & observation

      • Astrometry
      • Background Star Elimination
      • Cislunar Moving Objects
      • Continuous Coverage (CP)
      • Earth Albedo
      • Ephemeris Correlation
      • Hot Pixel
      • Illumination Constraint
      • Image Registration
      • Image Stacking
      • Infrared Radiation
      • Lunar Glare Zone
      • Pointing Constraint
      • Quasi-zero Wind Layer
      • Segmentation Map
      • Shift-and-Add (SAA)
      • Sidereal Tracking
      • Signal-to-Noise Ratio (SNR)
      • Solar Radiation
      • Source Extraction
      • Synthetic Tracking
      • Zonal Wind
    • Military space doctrine

      • Anti-Satellite Test (ASAT)
      • Cislunar Space Situational Awareness
      • Civil-Military Integration
      • Competitive Endurance
      • Component Field Commands
      • Commander, Space Forces (COMSPACEFOR)
      • Counterspace Operations
      • Directed Energy Weapon (DEW)
      • Distributed Architecture
      • DOTMLPF-P Framework
      • Force Design
      • Force Development
      • Force Employment
      • Force Generation
      • Golden Dome
      • Kinetic Weapon
      • Mission Command
      • Mission Delta (MD)
      • Operational Test and Training Infrastructure (OTTI)
      • Persistent Detection Corridor (PDC)
      • Resilience Map
      • Resilient/Disaggregated Architecture
      • Space Domain Awareness (SDA)
      • Space Mission Task Force (SMTF)
      • Space Superiority
      • Space Force Generation Process (SPAFORGEN)
      • System Delta (SYD)
    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • Danuri Lunar Orbiter
      • General Dynamics Mission Systems
      • GITAI USA
      • Indian Space Research Organisation
      • Korea Aerospace Administration
      • Lockheed Martin
      • Northrop Grumman
      • Quindar
      • Raytheon Missiles & Defense
      • Sci-Tec
      • SpaceX
      • Satish Dhawan Space Centre SHAR
      • True Anomaly
      • Turion Space

Cislunar Navigation Prospects

Editor's source: Shangguan Yong, Zheng Peng, Zhang Hua, et al. Research on the Current State and Technology Development of Cislunar Space Navigation[J]. Telemetry and Remote Sensing, 2026.

Author: Tianjiang Talk

Editor's source: https://cislunarspace.cn

Development Evolution Direction

Cislunar navigation is evolving from ground-based systems to multi-constellation coordination networks, moving toward multi-source fusion architectures and extending into deep space.

From Ground-Based to Multi-Constellation Coordination Networks

Current GNSS systems, through high-sensitivity receiver extension services, can achieve meter-level positioning on cislunar transfer orbits. However, challenges such as signal attenuation and coverage blind spots on the far side of the Moon remain, making this approach only suitable for early low-cost missions.

In the future, a network will form comprising extended Earth GNSS, Queqiao-series relay satellites, cislunar DRO constellations, lunar orbital constellations, and lunar surface beacon stations operating in coordination. At the international level, NASA's Luna Navigation Service (LNS) constellation and ESA's Moonlight constellation will collaborate to achieve resource sharing and complementary capabilities. Domestically, the "Cislunar Lighthouse" system based on DRO constellations will be further expanded, integrating Queqiao relay satellites with Chang'e mission achievements to build a comprehensive navigation network covering cislunar space and supporting multi-mission coordinated operations.

Toward Multi-Source Fusion Architectures

Future cislunar navigation will develop in the direction of "high precision, high autonomy, multi-source fusion, and intelligence":

Precision: Through optimized signal processing algorithms and the deployment of lunar surface augmentation beacons, sub-meter positioning accuracy in near-lunar space and ten-meter-level accuracy on cislunar transfer orbits will be achieved.

Autonomy: AI-based intelligent navigation algorithms will be developed to achieve adaptive adjustment of navigation parameters and autonomous fault diagnosis, extending autonomous navigation duration from the current several days to several months.

Fusion: A multi-source fusion system combining "GNSS extension + lunar constellations + celestial navigation + laser ranging" will enhance system robustness.

Key Technical Challenges

Cislunar navigation faces three major technical challenges:

Unified Space-Time Reference: The Moon lacks an independent time standard. Currently, all national lunar missions use their own time scales converted to Coordinated Universal Time (UTC). Lunar surface time runs approximately 57.5 microseconds faster per Earth day than Earth surface time. This level of time difference poses severe challenges to the timing requirements of navigation systems. In terms of spatial reference, Earth uses the International Terrestrial Reference Frame (ITRF) while the Moon uses the International Lunar Reference System (ILRS), requiring connection to Earth's J2000.0 inertial coordinate system through coordinate transformations. Error accumulation during this conversion process degrades navigation accuracy.

Complex Environmental Interference: Celestial gravitational fields cause light bending, increasing celestial navigation observation errors by more than 30%. GNSS sidelobe signal power flux density on the lunar surface is only about 10⁻⁶ of that on Earth. Lunar terrain occlusion results in 100% signal blockage on the far side of the Moon and more than 40% in the south polar region. The space radiation environment causes performance degradation of navigation equipment electronic components.

High-Precision Navigation Under Long-Delay and Weak-Coverage Links: How to achieve smooth transitions between navigation technologies at different mission phases while ensuring positioning accuracy and enhancing system autonomy remains a key technical challenge.

International Cooperation Needs

Building cislunar navigation systems requires international cooperation to promote the establishment of a globally unified lunar space-time reference system, to coordinate and solve the unification of lunar timekeeping standards and spatial reference frames, and to avoid fragmented development of national technical systems. China can leverage its inherent advantages in the Beidou Satellite Navigation System and satellite laser ranging technology to proactively participate in international standard-setting for lunar navigation, providing unified navigation services for international lunar research stations.

Extension into Deep Space

The development of cislunar navigation technology will provide a technical foundation for deep space exploration at greater distances. Building on X-ray pulsar navigation and laser ranging technology, future navigation systems will gradually extend to deep space regions such as Mars and the asteroid belt. The cislunar navigation network will serve as a relay station for deep space exploration, providing orbital correction and precise positioning services for spacecraft, pushing the boundaries of human space exploration further into the cosmos.

Development Pathway Recommendations

Taking cislunar hybrid navigation as the core development direction, achieving rapid breakthroughs in weak-signal navigation, supported by inter-satellite links, and building lunar-specific navigation constellations over the long term, represents the optimal development pathway balancing technical feasibility, cost control, and mission requirements.

PhaseKey Focus Areas
Near-termGNSS weak-signal navigation (low cost, quick results, suitable for basic navigation and emergency backup)
Mid-termCislunar hybrid navigation (5-10 years, primary solution for crewed lunar landing and lunar scientific research station)
Long-termLunar navigation constellation (lunar base construction, resource development, sustained presence)

Related Concepts

  • GNSS Weak-Signal Navigation
  • Earth-Moon Hybrid Navigation
  • Lunar Navigation Constellation
  • Inter-Satellite Link Navigation
  • X-ray Pulsar Navigation
  • Distant Retrograde Orbit (DRO)

References

  • Shangguan Yong, Zheng Peng, Zhang Hua, et al. Research on the Current State and Technology Development of Cislunar Space Navigation[J]. Telemetry and Remote Sensing, 2026.
  • Cong Dianwei, Wu Fumei, Li Chonghui, et al. Technology and Research Progress of Autonomous Navigation for Cislunar Spacecraft[J]. Radio Engineering, 2025, 55(2): 317-322.
  • Dong Guangliang, Li Haitao, Hao Wanhong, et al. Construction and Technology Development of China's Deep Space TT&C System[J]. Journal of Deep Space Exploration, 2018, 5(2): 99-114.
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Last Updated: 6/5/26, 11:01 AM
Contributors: Hermes Agent, Cron Job, Ou Yang Jiahong
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