TY - JOUR
T1 - Robust station-keeping for Halo orbits via auxiliary-controller-independent Lyapunov-based model predictive control
AU - Yu, Zhitong
AU - Shang, Haibin
AU - Zhao, Zichen
AU - Dong, Yue
AU - Shi, Lusha
N1 - Publisher Copyright:
© 2025 Published by Elsevier B.V. on behalf of COSPAR.
PY - 2025
Y1 - 2025
N2 - This paper develops an enhanced robust Lyapunov-based model predictive control (LMPC) scheme for station-keeping of Halo orbits with consideration of bounded uncertainties and control constraints. This method integrates the idea of robust control Lyapunov function (RCLF) into nonlinear MPC to robustly stabilize the tracking error within the explicitly characterized stability region. Specifically, the RCLF dissipation condition is firstly derived to analyze the stabilizability of the system with undefined feedback control. This property allows to construct the control-law-independent robust controllable domain, inside which admissible control exists to stabilize the spacecraft under bounded uncertainties. Subsequently, a sampling-based search strategy is developed to estimate the robust controllable domain, thereby deriving two contraction constraints. By incorporating the two constraints, the enhanced LMPC can be formulated independently of specific auxiliary control laws, whose stability region is explicitly characterized and extended. It brings appealing advantages that alleviate hard-to-avoid conservatism in traditional methods, thus improving tracking performances. Theoretically, within the stability region, robust stability and recursive feasibility can be well guaranteed. Numerical simulations demonstrate that the enhanced LMPC can eventually stabilize spacecraft to Halo orbit under bounded uncertainties and control constraints. Compared with traditional methods, the proposed controller achieves a 3–5 times scale of stability region, and tracking errors are reduced by about 50%.
AB - This paper develops an enhanced robust Lyapunov-based model predictive control (LMPC) scheme for station-keeping of Halo orbits with consideration of bounded uncertainties and control constraints. This method integrates the idea of robust control Lyapunov function (RCLF) into nonlinear MPC to robustly stabilize the tracking error within the explicitly characterized stability region. Specifically, the RCLF dissipation condition is firstly derived to analyze the stabilizability of the system with undefined feedback control. This property allows to construct the control-law-independent robust controllable domain, inside which admissible control exists to stabilize the spacecraft under bounded uncertainties. Subsequently, a sampling-based search strategy is developed to estimate the robust controllable domain, thereby deriving two contraction constraints. By incorporating the two constraints, the enhanced LMPC can be formulated independently of specific auxiliary control laws, whose stability region is explicitly characterized and extended. It brings appealing advantages that alleviate hard-to-avoid conservatism in traditional methods, thus improving tracking performances. Theoretically, within the stability region, robust stability and recursive feasibility can be well guaranteed. Numerical simulations demonstrate that the enhanced LMPC can eventually stabilize spacecraft to Halo orbit under bounded uncertainties and control constraints. Compared with traditional methods, the proposed controller achieves a 3–5 times scale of stability region, and tracking errors are reduced by about 50%.
KW - Halo orbits
KW - Lyapunov-based model predictive control
KW - Robust control Lyapunov function
KW - Robust controllable domain
KW - Station-keeping
UR - https://www.scopus.com/pages/publications/105025229451
U2 - 10.1016/j.asr.2025.10.105
DO - 10.1016/j.asr.2025.10.105
M3 - Article
AN - SCOPUS:105025229451
SN - 0273-1177
JO - Advances in Space Research
JF - Advances in Space Research
ER -