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�������պ����ѧѧ�� 2006, Vol. 32 Issue (08) :881-884    DOI:
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���Ĵ�, �ֹ�ƽ*
�������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100083
Application of quaternion in ejection seat performance simulation
Feng Wenchun, Lin Guiping*
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� A new method of combined quaternion and Euler angle was proposed to solve the singularity problem of Euler angle velocity equation at large extent attitude movement and all-attitude angles and jumping problems for the limitary of attitude angle using quaternion method in ejection seat performance simulation. Quaternion definition and geometry meaning were described and quaternion movement equation was introduced. Calculation formula of quaternion integral initial values in simulation was put forward through quaternion to Euler angle conversion. The problem of attitude angle jumping and discontinuous in simulation was analyzed. Simulation based on certain seat model was executed. Compared simulation result with experiment data and compared the result with another simulation using single quaternion method, it was shown that this method combined the virtue of quaternion and Euler angle velocity equation could efficiently resolve the singularity of Euler angle velocity equation and could realize all-attitude angle in simulation.
Keywords�� ejection seat   ejection simulation   Euler angle   all-attitude angle   quaternion     
Received 2005-09-30;
About author: ���Ĵ�(1972-),��,����������,��ʿ��, chunfeng@ase.buaa.edu.cn.
���Ĵ�, �ֹ�ƽ.��Ԫ���ڵ����������ܷ����е�Ӧ��[J]  �������պ����ѧѧ��, 2006,V32(08): 881-884
Feng Wenchun, Lin Guiping.Application of quaternion in ejection seat performance simulation[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(08): 881-884
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2006/V32/I08/881
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