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�������պ����ѧѧ�� 2003, Vol. 29 Issue (1) :23-26    DOI:
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��ƽ, ����, ���ڻ�*
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Post��Stall Maneuver Control Law for Aircrafts with New Control Configuration
Zhang Ping, Wang Dong, Chen Zongji*
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics

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Abstract�� A post-stall maneuver control law for aircraft with new control surfaces and trust vectoring control is proposed. The air dynamical data table is operated by minimal mean-square value of the error between the air data and the combined continued functions. The 6 freedom nonlinear dynamical equations of the aircraft are predigested at static operating points by extended linearization which still possess nonlinear characters. The control laws of the inner closed-loop system and post-stall maneuver are obtained through using symbol operations design. Simulation result shows that the control law is effective for the post-stall maneuver design of modern aircrafts.
Keywords�� non-linear control systems   flight control systems   thrust vector control   extended linearization   post-stall maneuver control     
Received 2001-07-06;
About author: �� ƽ(1950-),Ů,ɽ��ƽ����,������,100083,����.
��ƽ, ����, ���ڻ�.���������ַɻ��Ĺ�ʧ�ٿ��������[J]  �������պ����ѧѧ��, 2003,V29(1): 23-26
Zhang Ping, Wang Dong, Chen Zongji.Post��Stall Maneuver Control Law for Aircrafts with New Control Configuration[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(1): 23-26
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