[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
MISSILES AND GUIDANCE TECHNOLOGY

Design of UAV Attitude Controller Based on Fuzzy PID

  • CHEN Peng ,
  • DUAN Fengyang ,
  • ZHANG Qingjie ,
  • ZHENG Zhicheng ,
  • XIAO Wei
Expand
  • Department of Aviation Controlling, Aviation University of Air Force, Changchun 130022, China

Received date: 2014-02-10

  Online published: 2025-05-26

Abstract

The design of adaptive fuzzy PID UAV attitude control uses common PID control method and fuzzy control algorithm, since the membership function is over dependent on expert experience; genetic algorithm is used to optimize the membership function, the optimal control effect. The dynamic performance and robustness of the controller are greatly improved compared with traditional attitude controller, which is proved by simulation.

Cite this article

CHEN Peng , DUAN Fengyang , ZHANG Qingjie , ZHENG Zhicheng , XIAO Wei . Design of UAV Attitude Controller Based on Fuzzy PID[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(1) : 9 -11,18 . DOI: 10.15892/j.cnki.djzdxb.2015.01.003

[an error occurred while processing this directive]

References

[1]
Chen G. Conventional and fuzzy PID controllers: An overview International Journal of Intelligent Control and Systems, 1996 1(1):235-246.
[2]
鲁道夫. 布罗克豪斯. 飞行控制[M]. 金长江, 译. 北京: 国防工业出版社, 1999.
[3]
刘金锟. 智能控制[M]. 2版. 北京: 电子工业出版社, 2012.
[4]
吴森堂, 费玉华. 飞行控制系统[M]. 北京: 北京航空航天大学出版社, 2005.
[5]
文传源. 现代飞行控制系统[M]. 北京: 北京航空航天大学出版社, 2004.
[6]
胡寿松. 自动控制原理[M]. 5版. 北京: 科学出版社, 2007.
[7]
E Nakamura. Optimization of fuzzy membership function parameters[C]// IEEE International Conference on Systems, Man and Cybernetics, 1995 Intelligent Systems for the 21st Century, 1995.
[8]
薛定宇. 控制系统计算机辅助设计——MATLAB 语言及应用[M].2版. 北京: 清华大学出版社, 2006.
Outlines

/

[an error occurred while processing this directive]