TY - JOUR
T1 - Impulsive Station-Keeping Strategy for Libration Point Orbits via Nondivergent Component Suppression
AU - Du, Bohao
AU - Zhao, Wenchi
AU - Chen, Zhaoyue
AU - Bai, Xue
AU - Xu, Ming
AU - Jiang, Jun
AU - Liu, Jizhong
N1 - Publisher Copyright:
© 2025 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2025/9
Y1 - 2025/9
N2 - 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.
AB - 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.
KW - Celestial Mechanics
KW - Energy Economics
KW - Flight Testing
KW - Mechanical and Structural Vibrations
KW - Monte Carlo Simulation
KW - Numerical Integration
KW - Orbital Property
KW - Planets
KW - Space Orbit
KW - Structural Kinematics and Dynamics
UR - https://www.scopus.com/pages/publications/105015135846
U2 - 10.2514/1.G009001
DO - 10.2514/1.G009001
M3 - 文章
AN - SCOPUS:105015135846
SN - 0731-5090
VL - 48
SP - 2065
EP - 2076
JO - Journal of Guidance, Control, and Dynamics
JF - Journal of Guidance, Control, and Dynamics
IS - 9
ER -