| 某战术导弹舵机系统BIT分析 |
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| 引用本文： | 王丽娟.某战术导弹舵机系统BIT分析[J].航空兵器,2008(6). |
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| 作者姓名： | 王丽娟 |
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| 作者单位： | 中国空空导弹研究院,河南,洛阳,471009 |
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| 摘 要： | 针对日益复杂的武器系统故障检测难题,设计了某战术导弹舵机系统BIT。本文首先对舵机系统BIT进行了分析,然后介绍了其设计原理,并提出了减少BIT虚警的措施,最后进行了可测试性预计。该预计结果表明,舵机系统BIT故障检测率符合设计要求。
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| 关 键 词： | 测试性 机内测试 舵机 故障检测率 战术导弹 |
BIT Analysis of Control Actuator System on a Tactical Missile |
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| WANG Li-juan.BIT Analysis of Control Actuator System on a Tactical Missile[J].Aero Weaponry,2008(6). |
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| Authors: | WANG Li-juan |
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| Abstract: | To solve the problem of increasing complicated fault detect of weapon systems,the BIT of control actuator system is designed.This paper analyzes the BIT of control actuator firstly,then introduces its design principle and put forward the measure of decreasing BIT false alarm,at last carries the prediction of testability.The prediction result shows that the fault detection rate of BIT on control actuator satisfies the design requirement. |
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| Keywords: | testability built-in test control actuator system fault detection rate tactial missile |
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