Media type: E-Article Title: Finite-Time Attitude Optimization Maneuver Control for Coupled Spacecraft Under Attitude Measurement Errors and Actuator Faults Contributor: Zhang, Xiuyun; Zong, Qun; Dou, Liqian; Tian, Bailing; Liu, Wenjing imprint: Institute of Electrical and Electronics Engineers (IEEE), 2023 Published in: IEEE Transactions on Systems, Man, and Cybernetics: Systems Language: Not determined DOI: 10.1109/tsmc.2022.3221618 ISSN: 2168-2216; 2168-2232 Origination: Footnote: