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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
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      • Lift-to-Drag Ratio
      • Load Factor
      • Longitudinal and Lateral Motion
      • Lunar Lander
      • Minimum Energy Trajectory
      • Near-space
      • Newton's Iteration Method
      • Nuri (KSLV-II)
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      • Optimal Velocity Inclination
      • Orbit Capture
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      • 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
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      • Solar Exposure Factor
      • Specific Angular Momentum
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      • Stagnation Heat Flux
      • Standard Atmosphere
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      • 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
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      • 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
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      • Reduced-Order Dynamic Equations
      • Regional Station-keeping Control
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      • 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
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      • 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
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      • 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
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      • Low Prograde Orbit (LoPO)
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      • Lyapunov Orbit
      • Multi-Revolution Halo Orbit
      • Near-Rectilinear Halo Orbit (NRHO)
      • Orbit Identification
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      • Parking Orbit
      • Perilune
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      • Primary Impulse Orbit Transfer
      • Prograde
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      • Retrograde
      • Short Period Orbit
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      • 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
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      • Image Registration
      • Image Stacking
      • Infrared Radiation
      • Lunar Glare Zone
      • Pointing Constraint
      • Quasi-zero Wind Layer
      • Segmentation Map
      • Shift-and-Add (SAA)
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      • Signal-to-Noise Ratio (SNR)
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      • Synthetic Tracking
      • Zonal Wind
    • Military space doctrine

      • Anti-Satellite Test (ASAT)
      • Cislunar Space Situational Awareness
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      • Force Generation
      • Golden Dome
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      • 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

Poincaré Map

Author: CislunarSpace

Website: https://cislunarspace.cn

Definition

A Poincaré Map is a visualization method that reduces a continuous dynamical system to a discrete mapping. Its basic idea is to select a lower-dimensional cross-section in phase space (called a Poincaré Section) and record the state points each time the orbit crosses this section, transforming the continuous orbital evolution into a distribution of discrete points on the section. The Poincaré Map is named after the French mathematician Henri Poincaré and is a vital tool for analyzing nonlinear dynamical systems, identifying periodic orbits, and detecting chaotic behavior.

In the study of cislunar Distant Retrograde Orbit (DRO) families, Poincaré Maps are used to display the distribution characteristics of perilunes for family members in phase space, thereby revealing structural patterns of the orbit family and windows useful for transfer design.

Core Elements

Relationship with Poincaré Section

The Poincaré Map and Poincaré Section are closely related but have different emphases:

ConceptEmphasisDescription
Poincaré SectionGeometric objectAn (N−1)(N-1)(N−1)-dimensional or (N−2)(N-2)(N−2)-dimensional hyperplane in phase space
Poincaré MapMapping and visualizationThe distribution diagram of orbit crossing points on the section

In short, the Poincaré Section is the "cutting plane," and the Poincaré Map is the "pattern seen when projecting onto that plane."

Mathematical Definition

Given a continuous dynamical system x˙=f(x)\dot{\mathbf{x}} = \mathbf{f}(\mathbf{x})x˙=f(x), x∈RN\mathbf{x} \in \mathbb{R}^Nx∈RN, select a section Σ⊂RN−1\Sigma \subset \mathbb{R}^{N-1}Σ⊂RN−1. The First Return Map P:Σ→ΣP: \Sigma \to \SigmaP:Σ→Σ is defined as:

P(xk)=xk+1P(\mathbf{x}_k) = \mathbf{x}_{k+1} P(xk​)=xk+1​

where xk\mathbf{x}_kxk​ is the state at the kkk-th crossing of Σ\SigmaΣ, and xk+1\mathbf{x}_{k+1}xk+1​ is the state at the next crossing. This mapping is the Poincaré map, and its graphical representation is the Poincaré Map.

Physical Meaning of Crossing Point Patterns

The distribution patterns of discrete points in a Poincaré Map reflect the dynamical nature of the orbit:

Crossing PatternCorresponding Orbit Type
Isolated points (finite number)Periodic orbit (period is an integer multiple of the crossing count)
Closed curvesQuasi-periodic orbit (orbit on a torus)
Dense scattered points filling a regionChaotic orbit
Sparse scattered pointsLong-period orbit or transitional orbit

Application to DRO Orbit Families

Wei et al. (2026) used Poincaré Maps in their study of cislunar DRO orbit families to display the perilune distribution of each DRO member:

  1. Section selection: Using the perilune (r=rminr = r_{\text{min}}r=rmin​) as the section, recording the state (r,vr,vt)(r, v_r, v_t)(r,vr​,vt​) or its projection each time the orbit passes through the perilune
  2. Family member marking: Plotting the perilunes of DRO orbits with different periods on the same Poincaré Map
  3. Transfer window identification: Observing the density and directional characteristics of perilune distributions on the Poincaré Map to identify windows suitable for powered lunar flyby injection

For a single DRO orbit, since DRO is a periodic orbit, its perilune appears as fixed discrete points on the Poincaré Map. The overall distribution of the DRO orbit family on the Poincaré Map exhibits a regular curvilinear structure, reflecting the continuous variation of perilune states with orbital parameters (such as period).

Classical Applications in Low-Dimensional Systems

In two-dimensional autonomous systems, the Poincaré Map reduces to a sequence of points on a one-dimensional section, offering the most intuitive visualization:

  • Center-type fixed points: Correspond to stable periodic orbits, with surrounding points forming closed rings
  • Saddle-type fixed points: Correspond to unstable periodic orbits (e.g., Lyapunov orbits), with surrounding points arranged along stable/unstable manifolds
  • Invariant tori: Closed curves on the section, corresponding to quasi-periodic motion

In the planar restricted CR3BP, Poincaré Maps are commonly used to display crossing point distributions on the xxx-axis crossing section (y=0y = 0y=0, y˙>0\dot{y} > 0y˙​>0), distinguishing different orbit family types and chaotic regions.

Key Numerical Implementation Considerations

Producing high-quality Poincaré Maps requires attention to:

  • Propagation accuracy: Long-duration propagation requires high-precision integrators (e.g., Runge-Kutta 8(9) or symplectic integrators)
  • Crossing detection: Detect crossing times through sign changes, then interpolate for precise crossing points
  • Coordinate selection: Choose section coordinates that make different orbit family features most visible
  • Sufficient propagation time: Chaotic orbits require enough propagation time to reveal their scattering characteristics

Application Value

The core value of Poincaré Maps in cislunar space dynamics research lies in:

  • Orbit Family Structure Visualization: Reducing the high-dimensional phase space orbit family relationships to a 2D diagram, intuitively displaying topological relationships within the family
  • Perilune Distribution Analysis: For DRO transfer design, Poincaré Maps clearly show the position and velocity direction distributions of different DRO orbit perilunes
  • Chaos Identification: By observing whether crossing points form regular patterns, quickly determining whether an orbit is in a chaotic state
  • Transfer Design Aid: Combined with orbit family data generated by continuation methods, Poincaré Maps provide an intuitive "map" for transfer window screening

Related Concepts

  • Poincaré Section
  • Circular Restricted Three-Body Problem (CR3BP)
  • Continuation
  • Differential Correction
  • Impulsive Maneuver
  • Invariant Torus
  • Chaotic Orbit

References

  • Wei Z, et al. Research on powered lunar flyby transfer injection to cislunar distant retrograde orbit families[J]. Journal of Beijing University of Aeronautics and Astronautics, 2026.
  • Poincaré H. Les méthodes nouvelles de la mécanique céleste[M]. Gauthier-Villars, 1892.
  • Parker T S, Chua L O. Practical Numerical Algorithms for Chaotic Systems[M]. Springer, 1989.
  • Hénon M. Numerical exploration of the restricted problem, V: Hill's case[J]. Astronomy and Astrophysics, 1969, 1: 223-267.
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Last Updated: 6/5/26, 11:01 AM
Contributors: Cron Job, Ou Yang Jiahong
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