Fuzzy Adaptive Adjusted Sliding Mold VSC for Designing Missile Attitude Control System

TANG  Yidong; LI  Xiaobing; QIAO  Pengpeng

doi:10.15892/j.cnki.djzdxb.2013.02.036

Journal of Projectiles, Rockets, Missiles and Guidance >

2013 , Vol. 33 >Issue 2: 15 - 18

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2013.02.036

MISSILES AND GUIDANCE TECHNOLOGY

Fuzzy Adaptive Adjusted Sliding Mold VSC for Designing Missile Attitude Control System

TANG Yidong ,
LI Xiaobing ,
QIAO Pengpeng

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The Air and Missile Defense Institute, Air Force Engineering University, Xi'an 710051, China

Received date: 2012-09-24

Online published: 2025-05-26

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Abstract

In this paper, a fuzzy adaptive adjusted mold variable structure control(VSC) approach was proposed by combining normal VSC with the theory of fuzzy control. This approach not only keeps good robustness and adaptively, but also decreases the chattering produced by sliding mold variable structure control. In case of given parameters, this approach is applied to the missile attitude control system and its effectiveness is shown via the result of simulation.

Key words： missile attitude control; fuzzy adaptive; variable structure control; chattering; robustness

Cite this article

TANG Yidong , LI Xiaobing , QIAO Pengpeng . Fuzzy Adaptive Adjusted Sliding Mold VSC for Designing Missile Attitude Control System[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(2) : 15 -18 . DOI: 10.15892/j.cnki.djzdxb.2013.02.036

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References

[1]	赵宏战, 周军. 防空导弹姿态控制系统终态滑模变结构设计计算机仿真[J]. 计算机仿真, 2009,26 (2): 73- 76.
[2]	胡龙兵, 李言俊. 一种改进的变结构制导律的设计与仿真[J]. 火力与指挥控制, 2010,35 (9): 193– 194.
[3]	戚京锋, 周凤岐. 最终滑动模态变结构导弹控制系统设计. 弹箭与制导学报, 2004,24 (3): 273– 275.
[4]	高为炳. 变结构控制理论基础[M]. 北京: 中国科学技术出版社, 1990.
[5]	张翼飞, 杨辉, 邓方林. 二阶系统模糊变结构控制器设计及稳定性分析系统工程与电子技术, 2005,27 (2): 312- 315.
[6]	陈佳实. 导弹制导和控制系统的分析与设计[M]. 北京: 宇航出版社, 1989.
[7]	刘金琨. 滑模变结构控制 MATLAB 仿真[M]. 2版. 北京: 清华大学出版社, 2012.
[8]	韩曾晋. 自适应控制[M]. 北京: 清华大学出版社, 1995.

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