[an error occurred while processing this directive]
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 1998, Vol. 24 Issue (5) :563-566    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
�����1, ����ƽ1, ����2*
1. �������պ����ѧ �����������Ӧ����ѧϵ;
2. �վ�����ѧԺ ������
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

Download: PDF (0KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ �������������������涯��ѧ�����΢��-���������-�����㷨; ̽���������涯��ѧȷ����ʧ�ٻ�������Ч��Ҫ������,�⹹���˽�һ�������ʧ�ٻ����ɻ���Ƽ��оݵ���ֵ����; �����涯��ѧ��ƻ�������ģ����зɿ�ϵͳ�����⻷����,�Ա���������ĸ��ӻ����켣.�ɻ����ٷ���ʾ����������ֵ�������������˼�����㷨�ǿ��е�.
Email Alert
�ؼ����� ������   ������   ���п���   ����Ч��Ҫ��   ��������ģ��     
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;


About author: ٠28�� ������ 100083 ����
�����, ����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
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y1998/V24/I5/563
Copyright 2010 by �������պ����ѧѧ��