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动能拦截器轨道修正能力的数值计算方法

郑丹

现代防御技术2017,Vol.45Issue(1):62-69,81,9.
现代防御技术2017,Vol.45Issue(1):62-69,81,9.DOI:10.3969/j.issn.1009-086x.2017.01.012

动能拦截器轨道修正能力的数值计算方法

Numerical Computation Method for Divert Ability of Exoatmospheric Interceptor

郑丹1

作者信息

  • 1. 酒泉卫星发射中心,甘肃兰州732750
  • 折叠

摘要

Abstract

The divert ability of exoatmospheric interceptor depends on its guidance and control system.The numerical computation method for divert ability is proposed for a guidance and control system.The divert ability is obtained by computing the biggest zero-effort miss distance which can be corrected by the interceptor during the terminal course.Simulation results show that this method can compute the di vert ability in cases of insufficient fuel load and sufficient fuel load.The numerical computation method is quick and simple and can meet the need of quick computation of divert ability.

关键词

动能拦截器/数值计算方法/拦截域/轨道修正能力/装药量/零控脱靶向量

Key words

kinetic kill vehicle (exoatmospheric interceptor)/numerical method/intercept field/divert ability/charge (fuel load)/zero-effort miss

分类

航空航天

引用本文复制引用

郑丹..动能拦截器轨道修正能力的数值计算方法[J].现代防御技术,2017,45(1):62-69,81,9.

现代防御技术

OACSTPCD

1009-086X

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