Collinear Lagrange Point
Author: Tianjiang Shuo
Website: https://cislunarspace.cn
Definition
The three collinear equilibrium points of the restricted three-body problem, lying on the line joining the two primary masses. At these points the Hessian of the effective potential is indefinite (saddle-type): repulsive along the line joining the primaries and attractive perpendicular to it. The Jacobi constant at a collinear point makes the Hill's region develop a 'neck', enabling orbits to transit between the two primaries. Conley's paper provides the first systematic topological analysis of orbits near these points.
Related Concepts
- Manifold Propagation
- Low Lunar Orbit, LLO
- Complex Periodic Orbit
- Orbital Transfer Stage
References
- Conley - 1968 - Low energy transit orbits in restricted 3-body problem
