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The design of nonlinear flight control system of hypersonic cruise vehicle based on nonlinear disturbance observer

  • Chengbin Lian
  • , Cheng Bai
  • , Zhang Ren
  • , Xingyue Shao
  • 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

Hypersonic vehicle's nonlinear dynamics system is highly nonlinear, multivariable coupled and includes uncertain parameters. To solve this problem, a new back stepping controller is designed based on nonlinear disturbance observer (NDO). The NDO is used to observe the disturbance of the system and the limitation of the disturbance can be unknown. Theoretical analysis is done to validate that the system satisfy control requirements and is uniformly ultimately bounded. The simulation results also show that the developed method is effective and deals with the problem of uncertain factors preferably.

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
1473-1476
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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