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

^*Corresponding author for this work

School of Automation

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

Research output: Contribution to journal › Article › peer-review

117 Citations (Scopus)

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.

Original language	English
Article number	7046441
Pages (from-to)	368-381
Number of pages	14
Journal	IEEE Transactions on Automation Science and Engineering
Volume	13
Issue number	1
DOIs	https://doi.org/10.1109/TASE.2014.2379615
Publication status	Published - Jan 2016

Keywords

Actuator saturations and faults
Adaptive control
Attitude tracking
Fast terminal sliding mode control (FTSMC)
Finite-time control

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10.1109/TASE.2014.2379615

Cite this

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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.",

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KW - Adaptive control

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KW - Finite-time control

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

Abstract

Keywords

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