@inproceedings{a82c0eb053d7471aaf6334320c9220be,
title = "Finite-time fault tolerant control for spacecraft using sliding mode method",
abstract = "The problem of spacecraft attitude tracking control for actuator faults/failures and external disturbances is addressed in this paper. Assuming that information on external disturbances is unknown, a finite time sliding mode (FTSM) control law is developed to handle actuator faults/failures. Under the constraint conditions including the actuator faults and external disturbance, stability analysis shows that the designed controller not only ensures the attitude tracking convergence in finite time, but also has superior to actuator fault tolerance. Finally, in order to illustrate the efficiency and robustness of the proposed control law, the numerical simulations are carried out for spacecraft under actuator faults and disturbances.",
keywords = "Attitude tracking, FTSM, Fault-tolerant, Robust control",
author = "Lijun Zhang and Yuanqing Xia and Ganghui Shen and Kunfeng Lu",
note = "Publisher Copyright: {\textcopyright} 2017 IEEE.; 43rd Annual Conference of the IEEE Industrial Electronics Society, IECON 2017 ; Conference date: 29-10-2017 Through 01-11-2017",
year = "2017",
month = dec,
day = "15",
doi = "10.1109/IECON.2017.8217135",
language = "English",
series = "Proceedings IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "6516--6520",
booktitle = "Proceedings IECON 2017 - 43rd Annual Conference of the IEEE Industrial Electronics Society",
address = "United States",
}