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Adaptive Multivariable Integral TSMC of a Hypersonic Gliding Vehicle with Actuator Faults and Model Uncertainties

Title:

Adaptive Multivariable Integral TSMC of a Hypersonic Gliding Vehicle with Actuator Faults and Model Uncertainties

Li, Peng, Yu, Xiang, Zhang, Youmin and Peng, Xiaoyan (2017) Adaptive Multivariable Integral TSMC of a Hypersonic Gliding Vehicle with Actuator Faults and Model Uncertainties. IEEE/ASME Transactions on Mechatronics . pp. 1-10. ISSN 1083-4435 (In Press)

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Official URL: http://dx.doi.org/10.1109/TMECH.2017.2756345

Abstract

This paper presents a fault-tolerant control (FTC) strategy for a hypersonic gliding vehicle (HGV) subject to actuator malfunctions and model uncertainties. The control-oriented model of the HGV is estabilished according to the HGV kinematic and aerodynamic models. A single-loop design for HGV FTC under actuator faults is subsequently developed, where newly developed multivariable integral terminal sliding mode control (TSMC) and adaptive techniques are integrated. The multivariable integral TSMC is capable of ensuring the finite-time stability of the closed-loop system in the presence of actuator malfunctions and model uncertainties, while the adaptive laws are employed to tune the control parameters in response to the HGV status. Simulation studies based on a six degree-of-freedom (DOF) nonlinear model of the HGV are illustrated to highlight the effectiveness of the developed FTC scheme.

Divisions:Concordia University > Gina Cody School of Engineering and Computer Science > Mechanical, Industrial and Aerospace Engineering
Item Type:Article
Refereed:Yes
Authors:Li, Peng and Yu, Xiang and Zhang, Youmin and Peng, Xiaoyan
Journal or Publication:IEEE/ASME Transactions on Mechatronics
Date:26 September 2017
Funders:
  • National Natural Science Foundation of China under Grants 61403407, 51575167, 61573282 and 61603130
  • Natural Sciences and Engineering Research Council of Canada (NSERC)
  • Natural Science Foundation of Shaanxi Province under Grant 2015JZ020
  • Open Project Program of the State Key Laboratory of High Performance Computing under Grants 201613-02
Digital Object Identifier (DOI):10.1109/TMECH.2017.2756345
Keywords:Actuator faults, hypersonic gliding vehicle, fault tolerant control, multivariable integral TSMC, control-oriented model, composite-loop design.
ID Code:983248
Deposited By: DANIELLE DENNIE
Deposited On:28 Nov 2017 14:09
Last Modified:18 Jan 2018 17:56
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