Finite-time tracking control of rigid spacecraft under actuator saturations and faults

Kunfeng Lu; Yuanqing Xia; Chunmei Yu; Hailiang Liu

doi:10.1109/TASE.2014.2379615

Finite-time tracking control of rigid spacecraft under actuator saturations and faults

Kunfeng Lu
, Yuanqing Xia^*
, Chunmei Yu
, Hailiang Liu

^*此作品的通讯作者

自动化学院

Beijing Institute of Technology
Beijing Aerospace Automatic Control Institute
National Key Laboratory of Science and Technology on Aerospace Intelligence Control
National University of Defense Technology

科研成果: 期刊稿件 › 文章 › 同行评审

119 引用（Scopus）

摘要

In this paper, an adaptive fast terminal sliding mode control 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. Rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law.

源语言	英语
期刊论文编号	7046441
页（从-至）	368-381
页数	14
期刊	IEEE Transactions on Automation Science and Engineering
卷	13
期	1
DOI	https://doi.org/10.1109/TASE.2014.2379615
出版状态	已出版 - 1月 2016

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abstract = "In this paper, an adaptive fast terminal sliding mode control 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. 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 = "Kunfeng Lu and Yuanqing Xia and Chunmei Yu and Hailiang Liu",

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AU - Yu, Chunmei

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KW - Actuator saturations and faults

KW - Adaptive control

KW - Attitude tracking

KW - Fast terminal sliding mode control (FTSMC)

KW - Finite-time control

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Finite-time tracking control of rigid spacecraft under actuator saturations and faults

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