Lyapunov Control for the Circular Restricted Three-Body Problem Using Normal Forms
Abstract
Lyapunov-based control laws have been widely studied for transfers between Keplerian orbits in the two-body problem. However, in the context of orbit transfers near the equilibrium points of the circular restricted three-body problem (CR3BP), there is a lack of significant literature. The present study introduces a Lyapunov-based controller for low-thrust orbital transfers in the CR3BP. The approach uses action-angle coordinates based on the Birkhoff normal form, which can be used as local orbital elements around the equilibrium points of a Hamiltonian system. For the unstable equilibrium points of the CR3BP, a strategy using a combination of Lyapunov-based and linear quadratic regulator controllers is presented to perform a stabilized orbital transfer. The performance of the proposed controller is then demonstrated by application to numerical examples of low-thrust orbital transfers around different equilibrium points of the CR3BP.
Fields of Study & Subjects
Spacecraft Dynamics and Control
Space Satellite Systems and Control
Control and Stability of Dynamical Systems
Publication details
- Journal / source
- Journal of Guidance Control and Dynamics
- Volume
- 49
- Issue
- 6
- Pages
- 1630–1644
- Publication date
- 5 March 2026
- Language
- EN