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导弹飞行试验快速判决系统设计

李鹏

舰船电子工程2018,Vol.38Issue(5):107-110,4.
舰船电子工程2018,Vol.38Issue(5):107-110,4.DOI:10.3969/j.issn.1672-9730.2018.05.025

导弹飞行试验快速判决系统设计

Rapid Decision System of Missile Flight Test

李鹏1

作者信息

  • 1. 92941部队 葫芦岛125001
  • 折叠

摘要

Abstract

Aiming to finish the large missile flight test in rang,the article designs the quick judge system.The system can fore-cast the impact point,judge the fault in the telemetry parameters,and compute the missile miss distance.The application of range test shows that the quick judge system has strong realtime and high accuracy.It can provide the real-time analysis report about whether the missile hit the target or not.There is a high reference value and broad application prospect in the filed of typical faults judgement.

关键词

指挥控制/导弹/快速判决

Key words

command and control/missile/rapid judgment

分类

信息技术与安全科学

引用本文复制引用

李鹏..导弹飞行试验快速判决系统设计[J].舰船电子工程,2018,38(5):107-110,4.

基金项目

国家自然科学基金项目(编号:61473285)资助. (编号:61473285)

舰船电子工程

OACSTPCD

1672-9730

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