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Anti-windup smooth switching controller design of morphing aircraft

  • Beihang University
  • Beijing Simulation Center
  • Shanghai Aerospace Control Technology Institute

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Considering the attitude-stabilization during the transformation process of morphing aircraft with the effect of large scale change of system dynamic and constrained actuator output amplitude, based on mode-dependent average dwell time approach, a design methodology of anti-windup smooth switching controller is proposed. First, a class of chained smooth switching system model is established, which can reflect aerodynamic coefficient transition of morphing aircraft in the transformation process more precisely and reduce conservatism of controller design. Based on the model, the sufficient condition to ensure the finite-time boundedness and robustness of chained smooth switching system can be obtained via the mode-dependent average dwell time approach. Finally, design of anti-windup compensation is proposed. Also, the problem of anti-windup controller design is translated to problem of optimization with linear matrix inequalities constraint. Finally, simulation results are given to demonstrate the efficiency of the proposed controller design approach.

源语言英语
主期刊名2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
出版商Institute of Electrical and Electronics Engineers Inc.
ISBN(电子版)9781538611715
DOI
出版状态已出版 - 8月 2018
活动2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 - Xiamen, 中国
期限: 10 8月 201812 8月 2018

出版系列

姓名2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018

会议

会议2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
国家/地区中国
Xiamen
时期10/08/1812/08/18

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