| 导弹飞控系统测试技术 |
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| 引用本文： | 黄永飞,彭欣洁.导弹飞控系统测试技术[J].弹箭与制导学报,2009,29(1). |
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| 作者姓名： | 黄永飞 彭欣洁 |
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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： | 在某型导弹飞控系统测试技术中,运用了两种测试技术,一是在飞控系统的嵌入式计算机中设计了一套先进的机内测试(BIT)方法,增加了飞控系统的可测性;二是在ATE设备中设计了一套科学的测试流程,使飞控系统的测试全面完整;尤其是当BIT与ATE相结合时,形成了一种互动式的测试方法,对飞控系统的电气性能、惯导性能、控制性能等都进行了测试,使ATE的测试覆盖率大大提高。
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| 关 键 词： | 飞控系统 测试性 BIT ATE |
The Test Technique of a Missile's Flight Control System |
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| HUANG Yongfei,PENG Xinjie.The Test Technique of a Missile's Flight Control System[J].Journal of Projectiles Rockets Missiles and Guidance,2009,29(1). |
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| Authors: | HUANG Yongfei PENG Xinjie |
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| Affiliation: | China Airborne Missile Academy;Henan Luoyang 471009;China |
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| Abstract: | In testing technique of a missile's flight control system,applying two kinds of testing technique.One is in embedded computer,designing an advance system of built-in-test(BIT),increase testability.The other is in ATE,designing a scientific test process,it makes test complete and thorough,especially when combining BIT with ATE,form an exchange test,and it can test in three functions:electrical properties,inertial navigation properties and control properties.Improve testing coverage of ATE system greatly. |
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| Keywords: | flight control system testability BIT ATE |
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