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Autopilot design for a side-jet missile based on MRVSS with an adaptive approach law

  • Jian Chen*
  • , Hugh H.T. Liu
  • , Zhang Ren
  • *此作品的通讯作者
  • Beihang University
  • University of Toronto

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The autopilot design of a side jet and aero-fin blending control air-to-air missile is discussed in this paper and a Model Reference Variable Sliding Structure (MRVSS) method is presented. The side jets are in the discontinuous on-off pulse forms which are different from the conventional continuous side jets. The control parameters are sought though Genetic Algorithm (GA). Further, a novel adaptive variable-rate exponential approach law is introduced to approach the sliding surface quickly. The proposed method is verified by simulations on a research side-jet missile model and it's convenient to be carried out on other multi-actuator applications which is meaningful in actual engineering.

源语言英语
主期刊名Proceedings of the 29th Chinese Control Conference, CCC'10
2293-2298
页数6
出版状态已出版 - 2010
活动29th Chinese Control Conference, CCC'10 - Beijing, 中国
期限: 29 7月 201031 7月 2010

出版系列

姓名Proceedings of the 29th Chinese Control Conference, CCC'10

会议

会议29th Chinese Control Conference, CCC'10
国家/地区中国
Beijing
时期29/07/1031/07/10

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