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�������պ����ѧѧ�� 2004, Vol. 30 Issue (05) :410-413    DOI:
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2. �������չ���ѧԺ, ��̨ 264001
Robust control based on quantitative feedback theory for flight simulator
Fu Qiang1, Er Lianjie1, Zhao Guorong2*
1. School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics�� Beijing 100083, China;
2. Navy Aeronautics Engineering Institute, Yantai 264001, China

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Abstract�� ��To design the robust control system for flight simulator with large parameter uncertainty, quantitative feedback theory (QFT) was employed. The principle and design process of QFT were presented. The feedback controller and prefilter were designed using QFT, which make up of the control system of a certain flight simulator. The experiment result shows that the system keeps up perfect tracking performance when the loads of the flight simulator are changed. It indicates robustness of the system. The comparison with PID control demonstrates that QFT control is able to reject the friction nonlinearity. The anti-disturbance ability of QFT is very good. The application to flight simulator of QFT is successful. It shows the engineering value of the control method.
Keywords�� robust control   flight simulator   quantitative feedback theory     
Received 2003-01-08;
About author: �� ǿ(1976-),��,������Ϫ��,��ʿ��, fuqiang999@yahoo.com.cn.
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��ǿ, ������, �Թ���.���ڶ����������۵ķ��з���ת̨³������[J]  �������պ����ѧѧ��, 2004,V30(05): 410-413
Fu Qiang, Er Lianjie, Zhao Guorong.Robust control based on quantitative feedback theory for flight simulator[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2004,V30(05): 410-413
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2004/V30/I05/410
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