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A method of hybrid neural network adaptive control for flight control system

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

2 引用 (Scopus)

摘要

It is difficult to establish accurate models for complex flight control systems, but neural network has arbitrary nonlinear approximation ability. In order to overcome modeling errors and disturbances, a method of hybrid flight control is proposed. Firstly, inverse model of the object is identified online through neural networks and the feedback linearization control system is reached. And then circle theorem is used to design linear robust controller to control the state variables follow the input. A dynamic longitudinal model of a high-performance aircraft is considered to demonstrate the effectiveness of the proposed control scheme. Simulation results show designed controllers are highly adaptive and anti-interference ability.

源语言英语
主期刊名2010 International Conference on Intelligent Computation Technology and Automation, ICICTA 2010
页160-163
页数4
DOI
出版状态已出版 - 2010
活动2010 International Conference on Intelligent Computation Technology and Automation, ICICTA 2010 - Changsha, 中国
期限: 11 5月 2010 → 12 5月 2010

丛书

姓名2010 International Conference on Intelligent Computation Technology and Automation, ICICTA 2010
卷1

会议

会议2010 International Conference on Intelligent Computation Technology and Automation, ICICTA 2010
国家/地区中国
市Changsha
时期11/05/10 → 12/05/10

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