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

^*Corresponding author for this work

Ordnance Engineering College

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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.

Original language	English
Title of host publication	Proceedings of the International Symposium on Test and Measurement
Pages	1379-1382
Number of pages	4
Publication status	Published - 2003
Externally published	Yes

Publication series

Name	Proceedings of the International Symposium on Test and Measurement
Volume	2

Cite this

@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",

}

Fuzzy Control Design with Gains Adaptively Adjusted for Flight Control System. / Zhang, Lihua; Qi, Xiaohui; Feng, Jing et al.
Proceedings of the International Symposium on Test and Measurement. 2003. p. 1379-1382 (Proceedings of the International Symposium on Test and Measurement; Vol. 2).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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.

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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

Abstract

Publication series

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