@inbook{8402e9bf42e14fdc99a3d81867021007,
title = "Finite-time tracking control of rigid spacecraft under actuator saturations and faults",
abstract = "In this chapter, an adaptive fast terminal sliding mode control law (AFTSMCL) is presented to resolve attitude tracking control problem for rigid spacecraft, which can provide finite-time convergence, strong robustness, and fault-tolerant control. A rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law.",
keywords = "Actuator saturations and faults, Adaptive control, Attitude tracking, Fast terminal sliding mode control (FTSMC), Finite-time control",
author = "Yuanqing Xia and Jinhui Zhang and Kunfeng Lu and Ning Zhou",
note = "Publisher Copyright: {\textcopyright} Springer Nature Singapore Pte Ltd 2019.",
year = "2019",
doi = "10.1007/978-981-13-1373-8\_8",
language = "English",
series = "Advances in Industrial Control",
publisher = "Springer International Publishing",
pages = "141--169",
booktitle = "Advances in Industrial Control",
address = "Switzerland",
}