Distributed attitude coordination control of multiple spacecraft systems based on state feedback and output feedback
Wenyu Li, Chenyue Ma, Lei Chen, Shujuan Chen · 2016
This paper is to design attitude coordination control strategies for multiple spacecraft by state feedback and output feedback. Based on Lyapunov theory and graph theory, first, bounded coordination synchronization controllers are developed by state feedback. Second, output feedback controllers are developed for coordination synchronization(i.e. without angular velocity feedback), it can guarantee spacecraft attitude reach to stable attitude. Finally, simulation results illustrate and visualize the effectiveness and feasibility of the proposed control technique.