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�������պ����ѧѧ�� 2003, Vol. 29 Issue (12) :1127-1129    DOI:
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Design of fuzzy flight control system based on LMI
Wang Yueping*
Flight Automatic Control Research Institute, Xi'an 710065, China

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ժҪ �����˷ɿ�ϵͳ��ģ��ģ��,ͨ���������Ծ��󲻵�ʽLMI(Linear Matrix Inequality)�õ���һ�ּȿɱ�֤ģ��ϵͳȫ�ֽ����ȶ����ܽ��ջ��������������������ģ������ϵͳ����Ʒ���.���ø÷�����Ƶ�����ģ���ɿ�ϵͳ�����˷����³������֤.���������������ϵͳ����ȶ�������ָ��Ҫ���Ҿ��нϺõ�³����.
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Abstract�� A fuzzy flight control system model was established. Through using linear matrix inequality, a design method was gained which guarantees the fuzzy system is global asymptotic stability and the poles were assigned to anticipant areas. The numerical simulations of a fuzzy flight control system designed by this method show the system possesses not only satisfactory performances but also strong robustness.
Keywords�� pole allocation   robustness   T-S fuzzy model   parallel distributed compensation     
Received 2003-06-20;
About author: ��ԾƼ(1974-),Ů,������Ҵ��,˶ʿ��, ypwang@facri.com.
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��ԾƼ.����LMI��ģ���ɿ�ϵͳ���[J]  �������պ����ѧѧ��, 2003,V29(12): 1127-1129
Wang Yueping.Design of fuzzy flight control system based on LMI[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(12): 1127-1129
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2003/V29/I12/1127
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