| 某型直升机惯导失效导致载机异常抖动故障分析 |
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| 引用本文： | 万荣根,王晓鹏.某型直升机惯导失效导致载机异常抖动故障分析[J].直升机技术,2012(4):59-60. |
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| 作者姓名： | 万荣根 王晓鹏 |
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| 作者单位： | 陆航驻景德镇地区代表室,江西景德镇,333002 |
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| 摘 要： | 简要介绍了某型直升机惯导在空中失效后出现载机抖动的故障现象，分析了惯导部件的工作原理，找出了故障发生的机理和原因，并制定了相应整改措施。
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| 关 键 词： | 直升机 惯导 故障分析 |
Malfunction Analysis of the Fault Jitter Phenomenon of XX Helicopter in the Case of Inertial Navigation System Failure |
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| Authors: | WAN Ronggen WANG Xiaopeng |
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| Institution: | (Army Aviation Department of the PLA General Staff Military Representative Office in Jingdezhen Region, Jingdezhen 333002,China) |
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| Abstract: | This paper briefly introduced the fault jitter phenomenon of XX helicopter in the case of airborne inertial navigation system failure, analyzed the working principle of the inertial navigation system, found the reason of the fault phenomenon, developed some corrective measures. |
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| Keywords: | helicopter inertial navigation system malfunction analysis |
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