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Design of robust controller based on adaptive backstepping and slide mode for flight simulator

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Considering unknown nonlinearities, external disturbances and parameter perturbations existing in the flight simulator, A backstepping and slide mode controller is designed for the flight simulator. Firstly, the dynamic model of the flight simulator is proposed by test. Secondly, the backstepping controller with friction parameter update law is deduced for this dynamic model. Finally, simulation results show that the output from the system can achieve asymptotic tracking of the given position reference signal and the aberration of velocity response under the control of common PID controller is overcome.

源语言英语
主期刊名Sixth International Symposium on Instrumentation and Control Technology
主期刊副标题Sensors, Automatic Measurement, Control, and Computer Simulation
DOI
出版状态已出版 - 2006
活动Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation - Beijing, 中国
期限: 13 10月 200615 10月 2006

出版系列

姓名Proceedings of SPIE - The International Society for Optical Engineering
6358 II
ISSN(印刷版)0277-786X

会议

会议Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation
国家/地区中国
Beijing
时期13/10/0615/10/06

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