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    • Home (overview)
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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)
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      • GPS Time
      • Gravitational Potential
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      • High Altitude Airship (HAA)
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      • Lagrangian Perturbation Equations
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      • Passive Hydrogen Maser (PHM)
      • Perturbation Motion
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      • Reentry Corridor
      • Reentry Phase
      • Repeat Ground Track Orbit
      • Reusable Launch Vehicle
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      • Solar Exposure Factor
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      • Subsatellite Track
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      • Thrust-to-Weight Ratio
      • Thrust
      • Total Angle of Attack
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      • Tsiolkovsky Rocket Equation
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      • Two-Body Problem
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      • 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)
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      • 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
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      • Ephemeris Model
      • Equinoctial Orbital Elements (Equinoctial Orbital Elements)
      • Earth Restricted Three-Body Problem (ERTBP)
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      • 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
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    • Mission orbits

      • Apolune
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      • Altitude Regulation
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    • Astronomy & observation

      • Astrometry
      • Background Star Elimination
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    • Military space doctrine

      • Anti-Satellite Test (ASAT)
      • Cislunar Space Situational Awareness
      • Civil-Military Integration
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      • Operational Test and Training Infrastructure (OTTI)
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    • Organizations

      • Anduril Industries
      • Booz Allen Hamilton
      • Danuri Lunar Orbiter
      • General Dynamics Mission Systems
      • GITAI USA
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      • Raytheon Missiles & Defense
      • Sci-Tec
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      • Satish Dhawan Space Centre SHAR
      • True Anomaly
      • Turion Space

Invariant Manifold (Invariant Manifold)

Author: Tianjiang Shuo

Reference: 钱霙婧(2014)《地月空间拟周期轨道上航天器自主导航与轨道保持研究》

Website: https://cislunarspace.cn

Definition

An invariant manifold is a core concept in dynamical systems theory, referring to sets that remain unchanged during system evolution. For Hamiltonian systems, invariant manifolds are geometric structures in phase space that preserve system properties.

In the restricted three-body problem, invariant manifolds describe the manifold structure around periodic and quasi-periodic orbits near libration points, serving as key tools for understanding libration point dynamics and designing low-energy transfer orbits.

Stable and Unstable Manifolds

Stable Manifold

The stable manifold WsW^sWs refers to trajectories that, starting from any point on this manifold, asymptotically converge to the target periodic orbit or equilibrium point as t→+∞t \to +\inftyt→+∞:

Ws(x0)={x∈M:lim⁡t→+∞ϕt(x)=x0}W^s(x_0) = \{ x \in \mathcal{M} : \lim_{t \to +\infty} \phi^t(x) = x_0 \} Ws(x0​)={x∈M:t→+∞lim​ϕt(x)=x0​}

For collinear libration points (L₁, L₂, L₃), stable manifolds correspond to trajectories converging to the libration point along the unstable characteristic direction.

Unstable Manifold

The unstable manifold WuW^uWu refers to trajectories that, starting from any point on this manifold, asymptotically converge to the target periodic orbit or equilibrium point as t→−∞t \to -\inftyt→−∞:

Wu(x0)={x∈M:lim⁡t→−∞ϕt(x)=x0}W^u(x_0) = \{ x \in \mathcal{M} : \lim_{t \to -\infty} \phi^t(x) = x_0 \} Wu(x0​)={x∈M:t→−∞lim​ϕt(x)=x0​}

For collinear libration points, unstable manifolds correspond to trajectories diverging from the libration point along the unstable characteristic direction.

Dynamic Characteristics

Manifold Structure of Libration Points

Collinear libration points (L₁, L₂, L₃) have a saddle×center×center dynamical structure:

DirectionStabilityCorresponding Manifold
Crossing directionSaddle (unstable)One-dimensional unstable manifold
In-plane perpendicular to lineCenter (stable)Two-dimensional stable/unstable manifold
Perpendicular to orbital planeCenter (stable)Two-dimensional stable/unstable manifold

Geometric Form of Manifolds

Stable and unstable manifolds form "tube-like" structures in phase space:

  • Stable manifold tubes: Starting near periodic orbit, spiraling inward to periodic orbit
  • Unstable manifold tubes: Starting near periodic orbit, diverging outward

These tube structures constitute the main body of the Interplanetary Superhighway.

Application in Orbit Design

Low-Energy Transfer Orbit Design

Invariant manifolds can be used to design low-energy transfer orbits:

  1. Stable manifold transfer: Starting from target orbit, propagate outward along stable manifold to find intersection with departure orbit
  2. Unstable manifold transfer: Starting from departure orbit, converge inward along unstable manifold to target orbit

Libration Point Orbit Generation

When designing periodic orbits near libration points:

  1. Calculate initial estimate of periodic orbit in CR3BP model
  2. Use stable/unstable manifolds to verify orbit stability
  3. Use invariant manifolds as convergence directions for orbit design

Weak Stability Boundary (WSB) Transfer

Belbruno's Weak Stability Boundary theory is built on invariant manifolds: WSB transfer utilizes the natural diffusion effect of unstable manifolds to achieve orbital transfer with extremely small energy cost.

Application in Orbit Keeping

Manifold Stability Analysis

By analyzing the relative positions of stable and unstable manifolds around periodic orbits, long-term orbital stability can be determined:

  • Non-intersecting manifold tubes: Orbit may be stable
  • Intersecting manifold tubes: Orbit exhibits chaotic behavior

Control-Point Method

The control-point method for orbit keeping is essentially controlling spacecraft to return to periodic orbit along stable manifolds.

Related Concepts

  • Libration Point
  • Circular Restricted Three-Body Problem (CR3BP)
  • Weak Stability Boundary (WSB)
  • Halo Orbit
  • Low Energy Transfer Orbit

References

  • Koon W S, Lo M W, Marsden J E, et al. Dynamical systems, the three-body problem and space mission design[M]. 2011.
  • 钱霙婧. 地月空间拟周期轨道上航天器自主导航与轨道保持研究[D]. 哈尔滨工业大学, 2014.
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Last Updated: 6/5/26, 11:01 AM
Contributors: Cron Job, Ou Yang Jiahong
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