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

Yuanqing Xia; Jinhui Zhang; Kunfeng Lu; Ning Zhou

doi:10.1007/978-981-13-1373-8_8

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

Yuanqing Xia^*, Jinhui Zhang, Kunfeng Lu, Ning Zhou

^*此作品的通讯作者

自动化学院

科研成果: 书/报告/会议事项章节 › 章节 › 同行评审

6 引用（Scopus）

摘要

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.

源语言	英语
主期刊名	Advances in Industrial Control
出版商	Springer International Publishing
页	141-169
页数	29
DOI	https://doi.org/10.1007/978-981-13-1373-8_8
出版状态	已出版 - 2019

出版系列

姓名	Advances in Industrial Control
ISSN（印刷版）	1430-9491
ISSN（电子版）	2193-1577

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10.1007/978-981-13-1373-8_8

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Xia, Y., Zhang, J., Lu, K., & Zhou, N. (2019). Finite-time tracking control of rigid spacecraft under actuator saturations and faults. 在 Advances in Industrial Control (页码 141-169). (Advances in Industrial Control). Springer International Publishing. https://doi.org/10.1007/978-981-13-1373-8_8

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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",

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AU - Xia, Yuanqing

AU - Zhang, Jinhui

AU - Lu, Kunfeng

AU - Zhou, Ning

N1 - Publisher Copyright: © Springer Nature Singapore Pte Ltd 2019.

PY - 2019

Y1 - 2019

N2 - 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.

AB - 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.

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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BT - Advances in Industrial Control

PB - Springer International Publishing

ER -

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

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