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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

Poincaré Section

Source: Qiao et al. (2025) "Orbital parameter characterization and objects cataloging for Earth-Moon collinear libration points"

Website: https://cislunarspace.cn

Definition

A Poincaré Section (also called Poincaré map or surface of section) is a lower-dimensional cross-section formed by the intersection of a high-dimensional manifold in phase space with a designated hypersurface. It is used to visualize the dynamical structure of Hamiltonian systems and distinguish between different types of periodic and quasi-periodic orbits. In cislunar libration point research, the Poincaré section is the core tool for dimensional reduction and visualization of the 4D central manifold phase space.

Principles

For phase spaces with more than two dimensions, direct orbital visualization is impractical. The Poincaré section technique records the points where an orbit repeatedly crosses a lower-dimensional section. When the orbit's intersection points on the section form:

  • Closed curves: corresponding to quasi-periodic orbits (torus)
  • Isolated discrete points: corresponding to periodic orbits
  • Chaotic scatter points: corresponding to chaotic motion

Since Hamiltonian systems conserve energy, trajectories are confined to an N−1N-1N−1 dimensional energy surface. For the CR3BP collinear libration point central manifold (N=4N=4N=4), the Poincaré section is 2D.

Application to Cislunar Libration Points

Qiao et al. (2025) employ two types of sections:

1. θ2=0\theta_2 = 0θ2​=0 Section

Taking θ2=0\theta_2 = 0θ2​=0 as the section in central manifold coordinates (verified numerically to have the most frequent phase flow crossings). At a fixed energy level CCC, the section equation is:

HCM(I2,0,I3,θ3)=CH_{CM}(I_2, 0, I_3, \theta_3) = C HCM​(I2​,0,I3​,θ3​)=C

A uniform grid of points is selected on the section, initial conditions on the central manifold are computed and integrated, and crossing points are marked to produce the section diagram.

2. θ3=π/2\theta_3 = \pi/2θ3​=π/2 Section (Energy-Aggregate Section)

To display all orbit families (particularly the Halo orbit family at the torus center) on a single section, Qiao et al. (2025) select the θ3=π/2\theta_3 = \pi/2θ3​=π/2 section and overlay contour lines for different energy levels CCC, producing a "map" containing all orbit families near the libration point.

Orbit Family Signatures on the Section

On the θ3=π/2\theta_3 = \pi/2θ3​=π/2 section of Earth-Moon collinear libration points, different orbit families exhibit distinctly different geometric features:

Orbit FamilySection Signature
Lyapunov orbitIntersection curve with I3=0I_3 = 0I3​=0
Vertical Lyapunov orbitIntersection curve with I2=0I_2 = 0I2​=0
Lissajous orbitTrajectory fills the entire available region as θ3\theta_3θ3​ varies over [0,2π)[0, 2\pi)[0,2π)
Quasi-Halo orbitLocally forms toroidal structures
Halo orbitTorus shrinks to a point at specific I2,I3I_2, I_3I2​,I3​ values
Northern/Southern familyTwo toroidal structures centered at θ3=π/2\theta_3 = \pi/2θ3​=π/2 and θ3=3π/2\theta_3 = 3\pi/2θ3​=3π/2 respectively

Key Findings

  • At low energy levels, no Halo orbits exist in the section — this shows that Halo orbits originate from bifurcation of Lyapunov orbits as energy increases
  • Northern and southern Halo orbit families are indistinguishable on the θ3=π/2\theta_3 = \pi/2θ3​=π/2 section (symmetry); determining which family requires examining the θ3\theta_3θ3​ value
  • Near L3L_3L3​, neither Halo nor vertical Lyapunov orbits appear in the section because their bifurcation occurs far from the libration point (near Earth), where strong nonlinearity causes B-G expansion failure

Application to Orbit Identification

Qiao et al. (2025) develop the Poincaré section into a distribution map for libration point orbits, used for:

  1. Given an observed spacecraft state sequence, convert to characteristic parameters (I2,I3)(I_2, I_3)(I2​,I3​)
  2. Locate the nearest reference orbit on the section diagram
  3. Use optimization (Bayesian optimization) to find the reference orbit with minimum MSE

This method bypasses the difficulties of direct numerical integration in chaotic environments, achieving orbit identification through "map lookup."

Related Concepts

  • Central Manifold
  • Action-Angle Variables
  • Orbit Identification
  • Circular Restricted Three-Body Problem (CR3BP)
  • Invariant Torus
  • Bifurcation
  • Quasi-periodic Orbit

References

  • Arnol'd V I. Mathematical methods of classical mechanics[M]. Springer, 1989.
  • Qiao C, Long X, Yang L, et al. Orbital parameter characterization and objects cataloging for Earth-Moon collinear libration points[J]. Chinese Journal of Aeronautics, 2025. doi: 10.1016/j.cja.2025.103869.
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Last Updated: 4/29/26, 11:30 AM
Contributors: ouyangjiahong, Hermes Agent, Cron Job
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