Adaptive turbulence compensation for aircraft flight control

Liyan Wen, Gang Tao, Hao Yang, Yanjun Zhang*

*此作品的通讯作者

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

In this paper, a set of adaptive turbulence compensation techniques are investigated for aircraft flight control systems with different control gain matrices A(x), for which the multivariable adaptive disturbance rejection problems are formulated: one is for a nonsingular A(x), and one is for a singular A(x). Two unmatched disturbance rejection control design problems are addressed for the proposed aircraft turbulence compensation study: one with static feedback linearization under a direct control relative degree condition, and one with dynamic feedback linearization under an input extension control relative degree condition. For each problem, both nominal and adaptive turbulence compensation designs are developed for aircraft systems with known parameters and with unknown parameters, respectively. A typical aircraft application with turbulence disturbances is studied by a specific simulation study.

源语言英语
主期刊名CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference
出版商Institute of Electrical and Electronics Engineers Inc.
1612-1617
页数6
ISBN(电子版)9781467383189
DOI
出版状态已出版 - 20 1月 2017
已对外发布
活动7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016 - Nanjing, Jiangsu, 中国
期限: 12 8月 201614 8月 2016

出版系列

姓名CGNCC 2016 - 2016 IEEE Chinese Guidance, Navigation and Control Conference

会议

会议7th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2016
国家/地区中国
Nanjing, Jiangsu
时期12/08/1614/08/16

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