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MAV control system design based on virtual instrument

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A new design scheme of micro Rotorcraft Unmanned Aerial Vehicle (MRUAV) control system based on Virtual Instrument (VI) is developed in this paper. The control platform constructed by NI CompactRIO (a VI device) is used to realize the flight data acquisition, control algorithm design and control command transmission instead of the conventional flight controller. Considering the inaccuracy of the mathematical model and the adverse influence of high-frequency vibration, the Active Disturbance Rejection Controller (ADRC) not relying on the accurate mathematical model of controlled plant is selected as the control algorithm. The suitable ADRC parameters are recognized through successive approximation with the help of the online debugging function of VI. Finally, Flight experiments show the validity of the control system.

源语言英语
主期刊名2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
出版商Institute of Electrical and Electronics Engineers Inc.
474-479
页数6
ISBN(电子版)9781479946990
DOI
出版状态已出版 - 12 1月 2015
活动6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 - Yantai, 中国
期限: 8 8月 201410 8月 2014

出版系列

姓名2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014

会议

会议6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014
国家/地区中国
Yantai
时期8/08/1410/08/14

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