Design of missile autopilot with aerodynamic lift and reaction jets based on auto disturbance rejection controller

Chong Yang, Zhang Ke, Lu Mei Bai

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

First a new autopilot design model is presented for the interceptor missile with the blended aerodynamic lift and reaction jet. The reaction jet can improve the response speed, but the structure of control system becomes more complex. Therefore how to design control strategy properly is an urgent problem. Second, considering the discrete property of the lateral pulse jet thrusters and the continuous property of the aerodynamic fins, a kind of ADRC (active disturbance rejection control) autopilot system was designed for the aerodynamic lift/reaction jet missile. Finally, through a testing in the simulation of MATLAB, it is shown that, due to the sufficient utilization of the reaction jet, there is a significant improvement in the fast response and robust performance of the proposed controller. It is applicable to design the autopilot of aerodynamic lift and reaction jet blended missile.

源语言英语
主期刊名Advanced Manufacturing Technology
出版商Trans Tech Publications Ltd
1036-1039
页数4
ISBN(印刷版)9783037853702
DOI
出版状态已出版 - 2012
活动3rd international Conference on Manufacturing Science and Engineering, ICMSE 2012 - Xiamen, 中国
期限: 27 3月 201229 3月 2012

出版系列

姓名Advanced Materials Research
472-475
ISSN(印刷版)1022-6680

会议

会议3rd international Conference on Manufacturing Science and Engineering, ICMSE 2012
国家/地区中国
Xiamen
时期27/03/1229/03/12

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