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Adaptive tracking control of hypersonic re-entry vehicle with uncertain parameters

  • Chen Bai
  • , Chengbin Lian
  • , Zhang Ren
  • , Yao Fan
  • , Peng Qi
  • Beihang University
  • Second Artillery Representative Office in the Fourth Academy, CASC

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The problem of hypersonic re-entry vehicle attitude control with uncertain parameters is addressed. Aimed at a class of affine nonlinear system, adaptive control with observer is proposed. It is proved that observer error of uncertain parameters and tracking error of system output can uniformly asymptotically converge to zero. For implementation on hypersonic re-entry vehicle, two-loop attitude control is designed with aerodynamic derivatives considered as uncertain parameters. Simulations on 6DOF model of HRV show that the proposed adaptive control can keep good tracking performance in case of uncertain parameters.

源语言英语
主期刊名Proceedings - 3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013
出版商IEEE Computer Society
1594-1597
页数4
ISBN(印刷版)9780769551227
DOI
出版状态已出版 - 2013
活动3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013 - Shenyang, Liaoning, 中国
期限: 21 9月 201323 9月 2013

出版系列

姓名Proceedings - 3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013

会议

会议3rd International Conference on Instrumentation and Measurement, Computer, Communication and Control, IMCCC 2013
国家/地区中国
Shenyang, Liaoning
时期21/09/1323/09/13

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