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Modeling and robust adaptive attitude control of near space interceptor

  • Beihang University
  • China Airborne Missile Academy

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper establishes a precise model of near space interceptor with RCS and presents a robust adaptive attitude control law for it. Based on the normal model of the interceptor, this paper focuses on the analysis of all kinds of disturbance that may exist in the model, such as centroid drift and thrust misalignment, and gives the precise model of the disturbance. Then, the robust adaptive attitude control law is designed by using the back-stepping method and Nonlinear Extended State Observer(NESO). Back-stepping method is used to guarantee the system's stability and robustness, and NESO is used to estimate the integrated disturbance. The PWPF modulator is used to discretize the continuous control law. Finally, numerical simulations are performed using longitudinal attitude channel and the simulation results demonstrate the effectiveness of the attitude control law.

源语言英语
主期刊名Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016
出版商Institute of Electrical and Electronics Engineers Inc.
1663-1668
页数6
ISBN(电子版)9781467397148
DOI
出版状态已出版 - 3 8月 2016
活动28th Chinese Control and Decision Conference, CCDC 2016 - Yinchuan, 中国
期限: 28 5月 201630 5月 2016

出版系列

姓名Proceedings of the 28th Chinese Control and Decision Conference, CCDC 2016

会议

会议28th Chinese Control and Decision Conference, CCDC 2016
国家/地区中国
Yinchuan
时期28/05/1630/05/16

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