Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults

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 r...

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Published in:IEEE transactions on automation science and engineering 2016-01, Vol.13 (1), p.368-381
Main Authors: Lu, Kunfeng, Xia, Yuanqing, Yu, Chunmei, Liu, Hailiang
Format: Article
Language:English
Subjects:
Actuator saturations and faults
Actuators
adaptive control
Adaptive control systems
Attitude control
attitude tracking
Convergence
fast terminal sliding mode control (FTSMC)
Fault tolerance
finite-time control
Motors
Quaternions
Robust control
Robustness
Simulation
Space vehicles
Spacecraft
Terminals
Tracking control systems
Uncertainty
Vectors
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cited_by cdi_FETCH-LOGICAL-c326t-3af252473012dfde82d87e1de62e392a8d9c1ad17fe7721aa6a5d8246fbbbc203
cites cdi_FETCH-LOGICAL-c326t-3af252473012dfde82d87e1de62e392a8d9c1ad17fe7721aa6a5d8246fbbbc203
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container_title IEEE transactions on automation science and engineering
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creator Lu, Kunfeng
Xia, Yuanqing
Yu, Chunmei
Liu, Hailiang
description 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.
doi_str_mv 10.1109/TASE.2014.2379615
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subjects Actuator saturations and faults
Actuators
adaptive control
Adaptive control systems
Attitude control
attitude tracking
Convergence
fast terminal sliding mode control (FTSMC)
Fault tolerance
finite-time control
Motors
Quaternions
Robust control
Robustness
Simulation
Space vehicles
Spacecraft
Terminals
Tracking control systems
Uncertainty
Vectors
title Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults
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