Heteroclinic Connection
Author: Tianjiang Shuo
Contributing Institution: School of Astronautics, Harbin Institute of Technology, National Key Laboratory of Rapid Design and Intelligent Swarm of Small Spacecraft
Definition
A Heteroclinic Connection is a path formed by the intersection of invariant manifolds between two different periodic orbits in a dynamical system. Specifically, when the unstable manifold of one orbit coincides with the stable manifold of another orbit, a heteroclinic connection is formed — the spacecraft can naturally transition from one periodic orbit to another along this path without applying control thrust. In the Circular Restricted Three-Body Problem (CR3BP), heteroclinic connections widely exist between periodic orbits near the collinear libration points (L1, L2), serving as the core dynamical mechanism for designing low-energy transfer trajectories.
Core Elements
Mathematical Description
Let and be two distinct periodic orbits in the CR3BP, be the unstable manifold of , and be the stable manifold of . If a non-empty intersection exists:
then this intersection constitutes a heteroclinic connection from to . Along this connection, the orbit approaches as and approaches as .
Dynamical Characteristics
Heteroclinic connections have the following dynamical properties:
- Zero velocity increment: In the ideal CR3BP, a heteroclinic connection is an exact natural dynamical path requiring no propellant expenditure during transfer
- Sensitivity to perturbations: Heteroclinic connections exist at low-dimensional intersections within high-dimensional phase space, making them extremely sensitive to initial conditions and model parameters
- Energy matching constraint: The two periodic orbits must have identical Jacobi constants (energy); otherwise, the manifolds will not intersect
Typical Heteroclinic Connections
In the Earth-Moon system, typical heteroclinic connections include:
| Connection Type | Connected Objects | Characteristics |
|---|---|---|
| L1-L2 connection | L1 Halo ↔ L2 Halo | Connects collinear libration point regions on both sides of the Moon |
| L1-Lyapunov ↔ L2-Lyapunov | L1 planar orbit ↔ L2 planar orbit | Low-energy transfer channel within the orbital plane |
| Butterfly orbit internal connection | L1 Halo ↔ L2 Halo (large amplitude) | Butterfly orbits themselves embody heteroclinic connections |
Applications in Cislunar Space
Heteroclinic connections have significant application value in cislunar space mission design:
- Low-energy transfer trajectories: By concatenating heteroclinic connection segments, low-energy transfer trajectories from near-Earth orbit to orbits near the Moon can be designed, significantly reducing propellant requirements
- L1-L2 region interconnection: Heteroclinic connections provide natural dynamical channels between the Lunar Gateway and the far side of the Moon, supporting diverse mission topologies
- Formation reconfiguration: Using heteroclinic connections, formation spacecraft can collectively transfer from one periodic orbit to another, enabling global transformation of formation configurations
Related Concepts
- Butterfly Orbit
- Halo Orbit
- Lyapunov Orbit
- Low-energy Transfer
- Circular Restricted Three-Body Problem (CR3BP)
- Fuel-optimal Control
References
- Koon W S, Lo M W, Marsden J E, et al. Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics[J]. Chaos, 2000, 10(2): 427-469.
- 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.
