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Modeling and simulation of the helicopter control system based on the flight qualities

  • Cheng Wen Jian*
  • , Shu Li
  • , J. Zhang
  • *此作品的通讯作者
  • 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

Helicopter is a strong coupling and instability nonlinear system, of which the inherent flight qualities are poor. Helicopter model following control technology can make four control channels of helicopter with excellent tracking and decoupling characteristics. This paper applied the control method of model following control combining eigenststructure assignment to the helicopter control system. The results of simulation show that the helicopter flight qualities meet the requirements of ADS-33, the helicopter has excellent tracking and decoupling characteristics. Thus it proves that this control method is of great effectiveness.

源语言英语
主期刊名Materials, Transportation and Environmental Engineering II
编辑Jimmy C.M. Kao, Wen-Pei Sung, Ran Chen
出版商Trans Tech Publications Ltd
1493-1497
页数5
ISBN(电子版)9783038352488
DOI
出版状态已出版 - 2014
活动2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014 - Kunming, 中国
期限: 30 7月 201431 7月 2014

出版系列

姓名Advanced Materials Research
1030-1032
ISSN(印刷版)1022-6680
ISSN(电子版)1662-8985

会议

会议2nd International Conference on Materials, Transportation and Environmental Engineering, CMTEE 2014
国家/地区中国
Kunming
时期30/07/1431/07/14

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