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�������պ����ѧѧ�� 1998, Vol. 24 Issue (5) :563-566    DOI:
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Applications of Inverse Flight Dynamics
Zhang Shuguang1, Fang Zhenping1, Wang Yong2*
1. Beijing University of Aeronautics and Astronautics,Dept.of Flight Vehicle Design and Applied Mechanics;
2. Air Force College of Engineering, Section of Elementary Disciplines

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Abstract�� Two computational techniques for inverse fight dynamics, namely derivation-iteration and integration-iteration techniques, are investigated.The application of inverse dynamics to determine control power requirements for post-stall maneuvering is researched, and a maneuvering flight trajectory based algorithm is provided, which lays a numerical foundation for simplifying design criteria for post-stall aircraft.With the model of inverse dynamics employed, a flight control mode for the outermost loop of the control system, named maneuver generator, is designed to follow desired complicated maneuvering flight trajectories.An example of rapid heading-reversal maneuver and other numerical simulations show the feasibility of the algorithm and the design idea.
Keywords�� inverse problem   controllability   flight control   control power requirements   maneuver generator     
Received 1997-06-27;
Fund:

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�����, ����ƽ, ����.�����涯��ѧ��Ӧ��[J]  �������պ����ѧѧ��, 1998,V24(5): 563-566
Zhang Shuguang, Fang Zhenping, Wang Yong.Applications of Inverse Flight Dynamics[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 1998,V24(5): 563-566
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