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Aiming at reducing the communication path, a class of distributed finite-time state observers is designed. To speed up the convergence rate of the multiple spacecraft system, a fast nonsingular terminal sliding mode function is proposed. Moreover, an adaptive control term is proposed to suppress the impact of the external state-dependent disturbances and unknown time-varying inertia uncertainties. Further considering the actuator saturation owing to its physical limitations, a saturation function is designed. With the distributed finite-time observers, the fast nonsingular terminal sliding mode function, the adaptive update law and the saturation function, a distributed finite-time coordinated attitude tracking saturation controller is designed. Using the proposed controller, the follower can synchronize with the common leader with time-varying trajectory in finite time. Simulation results demonstrate the effectiveness of the designed controller. <\/jats:p>","DOI":"10.1142\/s0218126620502126","type":"journal-article","created":{"date-parts":[[2020,2,4]],"date-time":"2020-02-04T07:38:12Z","timestamp":1580801892000},"page":"2050212","source":"Crossref","is-referenced-by-count":9,"title":["Distributed Finite-Time Coordinated Attitude Tracking Control for Multiple Spacecraft with Actuator Saturation"],"prefix":"10.1142","volume":"29","author":[{"given":"Zhi","family":"Gao","sequence":"first","affiliation":[{"name":"College of Information Engineering, Yancheng Institute of Technology, Yancheng 224051, P. R. China"}],"role":[{"role":"author","vocabulary":"crossref"}]},{"ORCID":"https:\/\/orcid.org\/0000-0001-6156-1678","authenticated-orcid":false,"given":"Zhihao","family":"Zhu","sequence":"additional","affiliation":[{"name":"School of Electrical Engineering, Yancheng Institute of Technology, Yancheng 224051, P. R. 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