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�������պ����ѧѧ�� 2004, Vol. 30 Issue (02) :143-146    DOI:
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1. �������պ����ѧ ����ϵͳ����ϵ, ���� 100083;
2. �й��տյ����о�Ժ, ���� 471009
Study on reliability for flight control system under influence of thrust misalignment
Chen Yunxia1, Sun Yufeng1, Duan Chaoyang2*
1. Dept. of System Engineering of Engineering Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;
2. China Airborne Missile Academy, Luoyang 471009, China

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Abstract�� Thrust vector misalignment is an important factor, which causes trajectory scatter and affects missile reliability. In order to find design defect and enhance system reliability, the technique of integrated analysis of performance and reliability under the thrust's random misalignment was put forward. The disturbing moments were deduced and established. The algorithm process of reliability simulation, approach of implementation and formulas of computing reliability were given. The method was verified by X-missile's flight control system.
Keywords�� flight control system   missile   reliability simulation   thrust misalignment     
Received 2003-07-24;
About author: ����ϼ(1977-),Ů,���ջ�����,��ʿ��, cyx-2000@163.com.
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����ϼ, �����, �γ���.����ƫ��Ӱ���µķɿ�ϵͳ�ɿ����о�[J]  �������պ����ѧѧ��, 2004,V30(02): 143-146
Chen Yunxia, Sun Yufeng, Duan Chaoyang.Study on reliability for flight control system under influence of thrust misalignment[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2004,V30(02): 143-146
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http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2004/V30/I02/143
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