Fuzzy Control Design with Gains Adaptively Adjusted for Flight Control System

Lihua Zhang; Xiaohui Qi; Jing Feng; Jianbin Wei

Fuzzy Control Design with Gains Adaptively Adjusted for Flight Control System

Lihua Zhang^*
, Xiaohui Qi
, Jing Feng
, Jianbin Wei

^*此作品的通讯作者

Ordnance Engineering College

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

The use of fuzzy control method in designing the flight control systems for the unmanned aerial vehicle (UAV) was studied. The method incorporated the adaptive adjustment of fuzzy control gains with the changing input. The simulation results indicated towards the efficient nature of the method in controlling the flight states.

源语言	英语
主期刊名	Proceedings of the International Symposium on Test and Measurement
页	1379-1382
页数	4
出版状态	已出版 - 2003
已对外发布	是

出版系列

姓名	Proceedings of the International Symposium on Test and Measurement
卷	2

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链接到 Scopus 的出版物

引用此

@inproceedings{3c0e1528048b4b19b7be94f663296448,

title = "Fuzzy Control Design with Gains Adaptively Adjusted for Flight Control System",

abstract = "The use of fuzzy control method in designing the flight control systems for the unmanned aerial vehicle (UAV) was studied. The method incorporated the adaptive adjustment of fuzzy control gains with the changing input. The simulation results indicated towards the efficient nature of the method in controlling the flight states.",

author = "Lihua Zhang and Xiaohui Qi and Jing Feng and Jianbin Wei",

year = "2003",

language = "English",

series = "Proceedings of the International Symposium on Test and Measurement",

pages = "1379--1382",

booktitle = "Proceedings of the International Symposium on Test and Measurement",

}

TY - GEN

T1 - Fuzzy Control Design with Gains Adaptively Adjusted for Flight Control System

AU - Zhang, Lihua

AU - Qi, Xiaohui

AU - Feng, Jing

AU - Wei, Jianbin

PY - 2003

Y1 - 2003

N2 - The use of fuzzy control method in designing the flight control systems for the unmanned aerial vehicle (UAV) was studied. The method incorporated the adaptive adjustment of fuzzy control gains with the changing input. The simulation results indicated towards the efficient nature of the method in controlling the flight states.

AB - The use of fuzzy control method in designing the flight control systems for the unmanned aerial vehicle (UAV) was studied. The method incorporated the adaptive adjustment of fuzzy control gains with the changing input. The simulation results indicated towards the efficient nature of the method in controlling the flight states.

UR - https://www.scopus.com/pages/publications/0141425782

M3 - Conference contribution

AN - SCOPUS:0141425782

T3 - Proceedings of the International Symposium on Test and Measurement

SP - 1379

EP - 1382

BT - Proceedings of the International Symposium on Test and Measurement

ER -

Fuzzy Control Design with Gains Adaptively Adjusted for Flight Control System

摘要

出版系列

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指纹

引用此