Station-keeping of Halo Orbits using Convex Optimization-Based Receding Horizon Control

In this work, we propose a convex optimization-based receding horizon control method for the station-keeping control of halo orbit in Earth-Moon system. we leverage the advantages of convex optimization and receding horizon control and design the method under the high-fidelity ephemeris model, making it feasible to actual mission. Simulation results show that our method reaches low tracking errors and control consumption and produces better performances than linear quadratic regulation method.