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�������պ����ѧѧ�� 2003, Vol. 29 Issue (7) :598-601    DOI:
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�������պ����ѧ �����������Ӧ����ѧϵ, ���� 100083
Study of optimization method for flight path following
He Pei, Qu Xiangju, Wu Zhe*
Dept. of Flight Vehicle Design and Applied Mechanics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� Minimizing the tracking deviation between the real path and the referenced path can produce optimal following path, but it will bring a considerable oscillation of optimal control variables. In order to alleviate the considerable oscillation, a new integrated control method that combines the deviation with its differential was presented. The numerical application of the integrated control method demonstrates that the proposed method is effective and valid with respect to the possible oscillation of optimal control variables. Consequently, the precision performance of the flight path following is further realized.
Keywords�� flight path control   flight paths   flight control     
Received 2002-05-20;
About author: �� ��(1973-),Ů,�ӱ���Է��,��ʿ��, hepei509@sohu.com.
�����, ����.�������ٵ��Ż������о�[J]  �������պ����ѧѧ��, 2003,V29(7): 598-601
He Pei, Qu Xiangju, Wu Zhe.Study of optimization method for flight path following[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2003,V29(7): 598-601
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