Finite-Time Attitude Optimization Maneuver Control for Coupled Spacecraft Under Attitude Measurement Errors and Actuator Faults

Xiuyun Zhang, Qun Zong, LiQian Dou, Bailing Tian, Wenjing Liu. Finite-Time Attitude Optimization Maneuver Control for Coupled Spacecraft Under Attitude Measurement Errors and Actuator Faults. IEEE Transactions on Systems, Man, and Cybernetics, Part A, 53(5):3082-3091, May 2023. [doi]

Abstract

Abstract is missing.