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Title: Integral-type sliding mode fault-tolerant control for attitude stabilization of spacecraft
Authors: Zhu, Senqiang
Shen, Qiang
Wang, Danwei
Poh, Eng Kee
Issue Date: 2015
Source: Qiang, S., Wang, D., Zhu, S., & Poh, E. K. (2015). Integral-type sliding mode fault-tolerant control for attitude stabilization of spacecraft. IEEE Transactions on Control Systems Technology, 23(3), 1131-1138.
Series/Report no.: IEEE transactions on control systems technology
Abstract: Two fault-tolerant control (FTC) schemes for spacecraft attitude stabilization with external disturbances are proposed in this brief. The approach is based on integral-type sliding mode control strategy to compensate for actuator faults without controller reconfiguration. First, a basic integral-type sliding mode FTC scheme is designed so that sliding manifold can be maintained from the very beginning. Once the system enters the sliding mode, the dynamics of the closed-loop system with actuator fault is identical to that of the nominal healthy system. Second, the integral-type sliding mode fault-tolerant controller is incorporated with adaptive technique to accommodate actuator faults so that the required boundary information can be relaxed. The effectiveness of the proposed schemes against actuator faults is demonstrated in simulation.
ISSN: 1063-6536
DOI: 10.1109/TCST.2014.2354260
Schools: School of Electrical and Electronic Engineering 
Rights: © 2015 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. The published version is available at: [].
Fulltext Permission: open
Fulltext Availability: With Fulltext
Appears in Collections:EEE Journal Articles

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