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垂线偏差对弹道落点精度的影响分析

常晓华 蒋鲁佳 杨锐 张婕 丰海

国防科技大学学报2017,Vol.39Issue(4):1-5,5.
国防科技大学学报2017,Vol.39Issue(4):1-5,5.DOI:10.11887/j.cn.201704001

垂线偏差对弹道落点精度的影响分析

Analysis on effects of vertical deflection for trajectory impact accuracy

常晓华 1蒋鲁佳 1杨锐 1张婕 1丰海1

作者信息

  • 1. 北京宇航系统工程研究所,北京 100076
  • 折叠

摘要

Abstract

In view of the effects of the vertical deflection on trajectory impact accuracy, the influence mechanisms of the vertical deflection on the launching coordinate system, the initial parameter, the force during the flight, the control criteria of the program angle, and the trajectory parameter under the geocentric coordinate system were analyzed respectively by combining with the particle dynamics model of the ballistic vehicle.Then, the mathematical models of the effects of the vertical deflection were established.Furthermore, based on the given computing method of trajectory impact deflection and taking a flight trajectory as example, the impact errors under different geodetic latitude of launch point and different launch azimuth angle were presented quantitatively.The research is of great reference value in the aspect of the improvement of the impact accuracy for the ballistic vehicle.

关键词

垂线偏差/飞行弹道/落点精度

Key words

vertical deflection/trajectory/impact accuracy

分类

航空航天

引用本文复制引用

常晓华,蒋鲁佳,杨锐,张婕,丰海..垂线偏差对弹道落点精度的影响分析[J].国防科技大学学报,2017,39(4):1-5,5.

基金项目

国家部委基金资助项目(613222) (613222)

国防科技大学学报

OA北大核心CSCDCSTPCD

1001-2486

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