Lyapunov Control for the Circular Restricted Three-Body Problem Using Normal Forms

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.

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Publication Details

Journal
Journal of Guidance Control and Dynamics
Published
2026-03-04
DOI
https://doi.org/10.2514/1.g009558
Primary Topic
Spacecraft Dynamics and Control
Type
article
Field-Weighted Citation Impact
0.00
Controls
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article

Lyapunov Control for the Circular Restricted Three-Body Problem Using Normal Forms

Harshul Sharma, Christopher J. Damaren
Journal of Guidance Control and Dynamics
Spacecraft Dynamics and Control
article

Lyapunov Control for the Circular Restricted Three-Body Problem Using Normal Forms

Harshul Sharma, Christopher J. Damaren
article en

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.

Journal of Guidance Control and Dynamics
University of Toronto (CA)
Openalex Percentile: Top 34%
Spacecraft Dynamics and Control
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