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�������պ����ѧѧ�� 2005, Vol. 31 Issue (01) :36-40    DOI:
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�ܽ�, �����*
�������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100083
Implicit model following technique for aircraft configuration with multiple control surfaces
Zhou Jie, Zhang Shuguang*
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� The implicit model following technique, based on linear quadratic theory, was applied to design the flight control augmentation system (FCAS) of an aircraft with multiple control surfaces. The selection philosophy for the ideal model was investigated, which is based on the flight dynamics and the flying qualities requirements. The closed-loop design schemes were evaluated according to command following accuracy and ability to subdue effects of the atmospheric turbulences and other disturbances, where the structured singular value analysis method was adopted to evaluate robust stability and robust performance of the FCAS. The results show that the designed FCAS can subdue the turbulence and has good robust stability and adequate robust performance.
Keywords�� model following   flying quality   structured singular value analysis   aircraft with multiple control surfaces     
Received 2003-07-16;
About author: �� ��(1979-),��,�Ĵ�������,˶ʿ��, james zj2000@yahoo.com.cn.
�ܽ�, �����.������沼�ַɻ���ģ�͸��ٿ������[J]  �������պ����ѧѧ��, 2005,V31(01): 36-40
Zhou Jie, Zhang Shuguang.Implicit model following technique for aircraft configuration with multiple control surfaces[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2005,V31(01): 36-40
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2005/V31/I01/36
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