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飞控系统模糊控制器设计及稳定性分析
引用本文:谢振华,范训礼,曲建岭,王磊,耿昌茂.飞控系统模糊控制器设计及稳定性分析[J].飞行力学,2000,18(2):30-34.
作者姓名:谢振华  范训礼  曲建岭  王磊  耿昌茂
作者单位:1. 西北工业大学自动控制系,陕西,西安,710072
2. 海军航空工程学院青岛分院航空军械系,山东,青岛,266041
基金项目:“国家重点基础研究发展规划项目”专项经费资助!项目 ( G1 9980 3 0 4 1 7)
摘    要:建立了飞控系统的Takagi-Sugeno(T-S)模糊模型;给出了设计模糊状态反馈控制器,保证闭环系统全局渐近稳定、具有一定衰减率稳定的两个充分条件;提出了采用线性矩阵不等式(LMI)方法,将该充分条件转化为对线性矩阵不等式族寻求LMI可行解的凸优化问题,得到了稳定性分析和模糊状态反馈控制器设计的新方法。仿真结果表明,所提出的设计方法方便有效,控制器鲁棒性好。

关 键 词:飞控系统  T-S模糊模型  模糊控制器设计  稳定性
修稿时间::

Fuzzy controller design and stability analysis for flight control systems
XIE Zhen-hua,FAN Xun-li,QU Jian-ling,WANG Lei,GENG Chang-mao.Fuzzy controller design and stability analysis for flight control systems[J].Flight Dynamics,2000,18(2):30-34.
Authors:XIE Zhen-hua  FAN Xun-li  QU Jian-ling  WANG Lei  GENG Chang-mao
Institution:XIE Zhen hua 1,FAN Xun li 1,QU Jian ling 2,WANG Lei 1,GENG Chang mao 2
Abstract:Takagi Sugeno(T S) fuzzy model of flight control systems is established. The sufficient conditions of asymptotic stability and stability with decay rate for the closed loop systems via fuzzy state feedback controller are presented. Based on the technique of linear matrix inequality (LMI), a new approach of stability analysis and fuzzy state feedback controller design through converting the conditions to the equivalent LMI problems to find the feasible solutions for a set of linear matrix inequalities is proposed. Simulation results demonstrate that the approach is valid, and the robustness of control systems is nice.
Keywords:flight control system  Takagi  Sugeno fuzzy model  linear matrix inequality  fuzzy controller design  asymptotic stability
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