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�������պ����ѧѧ�� 2006, Vol. 32 Issue (10) :1141-1145    DOI:
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�������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100083
Integral inference method for missile hit accuracy
Fu Huimin*
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� An integral inference method for missile hit accuracy is presented. Combining the simulation results of missile hit accuracy and the miss distance experiment data, the method can totally infer the miss distance experiment data of missile in various launching conditions. Furthermore, it can establish the mean, the variance and the hit probability estimators, and give their confidence limits and intervals in each launching condition. Compared with traditional methods, this method not only has higher precision, but also solves the problem of missile fire accuracy, dispersion and hit probability assessment with only one miss distance experiment datum in a launching condition.
Keywords�� hit accuracy   miss distance   dispersion   hit probability   integral estimate   small sample   simulation     
Received 2006-05-22;
About author: ������(1956-),��,�㽭�����, "����ѧ�߽����ƻ�"��Ƹ����, fuhuimin@263.net.
������.�������о��������ƶϷ���[J]  �������պ����ѧѧ��, 2006,V32(10): 1141-1145
Fu Huimin.Integral inference method for missile hit accuracy[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(10): 1141-1145
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2006/V32/I10/1141
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