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Virtual flight simulation of the basic finner projectile based on fuzz control

  • 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 computational method of computational fluid dynamics (CFD) coupled with rigid body dynamics (RBD) and flight control system (FCS) is developed. In simulations of FCS, the robust and simpler fuzz control method is used instead of the usual PID method. Taking the control of pitching attitude as an example, virtual flight simulations of the basic finner projectile are presented. Simulation results show that this coupled method has the ability to simulate complex aircrafts' maneuver actions.

源语言英语
主期刊名2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
出版商Institute of Electrical and Electronics Engineers Inc.
494-497
页数4
ISBN(电子版)9781538633052
DOI
出版状态已出版 - 14 9月 2017
活动8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017 - Prague, 捷克共和国
期限: 22 7月 201725 7月 2017

出版系列

姓名2017 8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017

会议

会议8th International Conference on Mechanical and Aerospace Engineering, ICMAE 2017
国家/地区捷克共和国
Prague
时期22/07/1725/07/17

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