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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)
      • 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)
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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
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      • Precession
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      • Reentry Corridor
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      • 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
      • Stratospheric Airship
      • Subsatellite Track
      • Sun-Synchronous Orbit
      • Thrust-to-Weight Ratio
      • Thrust
      • Total Angle of Attack
      • Trajectory Equation
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      • 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
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      • 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
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      • Patch Point (Splicing Point)
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      • Poincaré Map
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      • Zero-Effort Miss (ZEM)
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    • Mission orbits

      • Apolune
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      • Altitude Regulation
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    • Astronomy & observation

      • Astrometry
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      • Shift-and-Add (SAA)
      • Sidereal Tracking
      • Signal-to-Noise Ratio (SNR)
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      • Synthetic Tracking
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    • Military space doctrine

      • Anti-Satellite Test (ASAT)
      • Cislunar Space Situational Awareness
      • Civil-Military Integration
      • Competitive Endurance
      • Component Field Commands
      • Commander, Space Forces (COMSPACEFOR)
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      • Operational Test and Training Infrastructure (OTTI)
      • Persistent Detection Corridor (PDC)
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      • 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

Butterfly Orbit

Author: Tianjiang Says

Website: https://cislunarspace.cn

Definition

A Butterfly Orbit is a large-amplitude three-dimensional periodic orbit family connecting the L1 and L2 libration points, belonging to a special category of Libration Point Orbits (LPO). Its name originates from the orbital shape in the rotating coordinate system — the orbit moves around both the L1 and L2 libration points, resembling a butterfly with spread wings. Butterfly orbits represent a relatively novel orbit family in the current cislunar space orbit classification system, embodying the connecting structures between different equilibrium regions in libration point dynamics.

Core Elements

Dynamical Characteristics of Butterfly Orbits

Butterfly orbits possess the following properties within the CR3BP framework:

  • Dual libration point connection: Butterfly orbits simultaneously encircle both the L1 and L2 collinear libration points, representing large-amplitude periodic solutions that connect these two dynamical regions
  • Large-amplitude motion: Unlike small-amplitude Lyapunov or Halo orbits confined to the vicinity of a single libration point, butterfly orbits span a much larger region of cislunar space
  • Three-dimensional periodicity: Butterfly orbits are strictly three-dimensional periodic orbits that close precisely in the rotating coordinate system
  • Complex symmetry: Butterfly orbits possess symmetry with respect to the yOzyOzyOz plane, forming mirror-image structures on either side of the Earth-Moon line

Classification of Butterfly Orbits

Butterfly orbits have been primarily found in the vicinity of the L1 and L2 libration points in the Earth-Moon system:

Orbit FamilyParent Libration PointCharacteristics
Butterfly L1L1/L2 connectionLarge-amplitude orbit encircling L1 and L2, resembling the left wing of a butterfly
Butterfly L2L1/L2 connectionLarge-amplitude orbit encircling L1 and L2, resembling the right wing of a butterfly

Relationship Between Butterfly Orbits and Other Libration Point Orbits

Butterfly orbits have profound dynamical connections with conventional libration point orbit families:

  • Relationship with Lyapunov/Halo orbits: Butterfly orbits can be viewed as new orbital structures that emerge through bifurcation as Lyapunov or Halo orbit families increase in amplitude
  • Relationship with heteroclinic connections: The existence of butterfly orbits is closely related to the heteroclinic connections between the L1 and L2 libration points, reflecting deep connections between the dynamical regions surrounding these points
  • Relationship with invariant manifolds: The invariant manifolds (stable and unstable manifolds) of butterfly orbits can be used to design low-energy transfer trajectories connecting the L1 and L2 regions

Stability Characteristics

The stability characteristics of butterfly orbits are relatively complex:

  • Due to their large spatial extent and connection of two unstable equilibrium points, butterfly orbits typically exhibit strong dynamical instability
  • High stability indices indicate that motion in the vicinity of butterfly orbits is extremely sensitive to initial conditions
  • Although the orbits themselves are unstable, their invariant manifold structures provide a theoretical foundation for designing controllable transfer trajectories

Application Value

Butterfly orbits have the following potential applications in cislunar space missions:

  • Rapid L1-L2 transfer: Butterfly orbits inherently connect the L1 and L2 regions, providing a natural dynamical corridor for designing direct transfers between these two points
  • Global dynamical research: Butterfly orbits offer an important window into the global phase space structure of cislunar space, particularly in studying the connection mechanisms between libration points
  • Complex mission trajectory design: Using butterfly orbits and their invariant manifolds, complex exploration mission trajectories covering multiple libration point regions can be designed
  • Orbit classification complement: As a new member of the libration point orbit family, butterfly orbits enrich the classification system of periodic orbits in cislunar space

Related Concepts

  • Halo Orbit
  • Lyapunov Orbit
  • Vertical Orbit
  • Axial Orbit
  • Heteroclinic Connection
  • Circular Restricted Three-Body Problem (CR3BP)

References

  • Guzzetti D, Bosanac N, Howell K C. A framework for efficient trajectory comparisons in the Earth-Moon design space[C]. AAS/AIAA Space Flight Mechanics Meeting, 2014.
  • Doedel E J, Romanov V A, Paffenroth R C, et al. Elemental periodic orbits associated with the libration points in the circular restricted 3-body problem[J]. International Journal of Bifurcation and Chaos, 2007, 17(8): 2625-2677.
  • Haapala A, Vaquero M, Pavlak T A, et al. Trajectory selection strategy for tours in the Earth-Moon system[C]. AAS/AIAA Astrodynamics Specialist Conference, 2013.
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Last Updated: 6/5/26, 11:01 AM
Contributors: Ou Yang Jiahong
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