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巡航导弹飞行撞地概率的一种计算方法
引用本文:湛必胜,王明海,李邦杰,王继平.巡航导弹飞行撞地概率的一种计算方法[J].飞行力学,2006,24(3):78-79,84.
作者姓名:湛必胜  王明海  李邦杰  王继平
作者单位:1. 北京航空航天大学,宇航学院,北京,100083
2. 第二炮兵工程学院603教研室,陕西,西安,710025
摘    要:研究了巡航导弹飞行高度控制系统对应的高度控制误差和地形起伏误差,在综合这两种误差的基础上,提供了一种飞行撞地概率的计算方法,并给出了飞行高度与之对应的撞地概率计算实例。计算和分析得出,参考航迹高度取现行标准值的某型巡航导弹撞地概率太大,需通过减小高度探测控制系统的误差或者增大参考航迹的规划高度来降低撞地概率。

关 键 词:巡航导弹  飞行高度  撞地概率
文章编号:1002-0853(2006)03-0078-02
收稿时间:2005-07-21
修稿时间:2005-07-212006-04-26

A Calculation Method of Bumping Ground Probability of Cruise Missle Flight
ZHAN Bi-sheng,WANG Ming-hai,LI Bang-jie,WANG Ji-ping.A Calculation Method of Bumping Ground Probability of Cruise Missle Flight[J].Flight Dynamics,2006,24(3):78-79,84.
Authors:ZHAN Bi-sheng  WANG Ming-hai  LI Bang-jie  WANG Ji-ping
Abstract:This paper studied height control error and terrain undulation error in relation to the height control system of cruise missile flight.A calculation method of bumping ground probability of the flight is presented and at the same time the calculation example of bumping ground probability in relation to flight height is also given in the paper.It is educed by calculation and analysis that bumping ground probability of some type of cruise missiles is too big when the reference track height takes the present standard value.It is necessary to reduce the bumping ground probability by reducing the error of a height detection control system or increasing the layout height of reference track.
Keywords:cruise missile  flight height  bumping ground probability  
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