Impulsive Station-Keeping Strategy for Libration Point Orbits via Nondivergent Component Suppression

  • Bohao Du
  • , Wenchi Zhao
  • , Zhaoyue Chen*
  • , Xue Bai
  • , Ming Xu
  • , Jun Jiang
  • , Jizhong Liu
  • *Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

Center manifold theory describes the phase flow near collinear libration points as a combination of two harmonic oscillations and one hyperbolic motion, the latter driving exponential spacecraft divergence. The Floquet modes approach (FMA), based on Floquet theory, is widely studied but suffers from inefficiency due to its inability to suppress nondivergent components (NDCs) beyond the unstable motion. To overcome this limitation, we propose an improved FMA strategy that leverages the collateral effect of NDCs—a key factor in traditional FMA failures yet exploitable for enhanced control. First, a predictor–corrector algorithm computes a correction factor κ to refine unstable mode estimation, accounting for unmodeled nonlinearities. Next, the most critical NDC is identified and suppressed, the timing of the next maneuver is predicted, and a maneuver overshoot factor δv is introduced to regulate excessive NDCs. By strategically selecting maneuver types, our approach ensures effective suppression. Finally, three numerical simulations validate the method’s effectiveness, versatility, and robustness.

Original languageEnglish
Pages (from-to)2065-2076
Number of pages12
JournalJournal of Guidance, Control, and Dynamics
Volume48
Issue number9
DOIs
StatePublished - Sep 2025

Keywords

  • Celestial Mechanics
  • Energy Economics
  • Flight Testing
  • Mechanical and Structural Vibrations
  • Monte Carlo Simulation
  • Numerical Integration
  • Orbital Property
  • Planets
  • Space Orbit
  • Structural Kinematics and Dynamics

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