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基于任务的舰空导弹武器系统可靠性试验设计

薛鲁强 褚政 李绅政

指挥控制与仿真2012,Vol.34Issue(4):120-123,4.
指挥控制与仿真2012,Vol.34Issue(4):120-123,4.DOI:10.3969/j.issn.1673-3819.2012.04.026

基于任务的舰空导弹武器系统可靠性试验设计

DOE of Ship-to-air Missile System's reliability on basic of Mission

薛鲁强 1褚政 1李绅政2

作者信息

  • 1. 海军航空工程学院指挥系,山东烟台264001
  • 2. 92493部队2分队,辽宁葫芦岛125000
  • 折叠

摘要

Abstract

This article focuses on operational mission and fight handling characteristics of ship-to-air missile, uses simulation experiment design method, sets ocean-going mission profile, takes influence research of ship-to-air missile system's and subsystem's reliability to missile weapon system fighting efficiency. Establishment simulation model and using model of ship-to-air missile weapon system and advances the index for the research. Setting the different combating applications A, B, C for the background and have numerical simulation analysis. The digital simulation results show the influence that the factors of reliability and the anticipated reliability growth to the fighting efficiency.

关键词

舰空导弹/可靠性/试验设计

Key words

ship-to-air missile/ reliability/ design of experiment

分类

军事科技

引用本文复制引用

薛鲁强,褚政,李绅政..基于任务的舰空导弹武器系统可靠性试验设计[J].指挥控制与仿真,2012,34(4):120-123,4.

指挥控制与仿真

OACSTPCD

1673-3819

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