| 某导弹系统随动异常机理分析与解决 |
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| 引用本文： | 李井还,王瑞峰. 某导弹系统随动异常机理分析与解决[J]. 测控技术, 2017, 36(5): 156-158. DOI: 10.3969/j.issn.1000-8829.2017.05.038 |
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| 作者姓名： | 李井还 王瑞峰 |
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| 作者单位： | 1. 中国空空导弹研究院,河南洛阳,471009;2. 中国人民解放军95835部队,新疆乌鲁木齐,841700 |
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| 摘 要： | 为排查和解决导弹系统大角度随动发生摆动的现象,从理论分析和计算中发现发射装置在大角度随动控制时,由于本身软硬件设计约束,控制算法溢出,会导致导引头随动异常.通过对发射装置软件控制算法采用压缩法处理后,导引头随动正常.经试验论证,此故障原因定位准确,改进设计方法有效,满足系统大角度随动要求.
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| 关 键 词： | 发射装置 大角度 随动 溢出 |
Analysis and Solution of Dynamic Mechanism for Abnormal Servo of A Missile System |
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| LI Jing-huan,WANG Rui-feng. Analysis and Solution of Dynamic Mechanism for Abnormal Servo of A Missile System[J]. Measurement & Control Technology, 2017, 36(5): 156-158. DOI: 10.3969/j.issn.1000-8829.2017.05.038 |
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| Authors: | LI Jing-huan WANG Rui-feng |
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| Abstract: | In order to troubleshoot and solve the dynamic swing for the missile system with large angle servo,through the theoretical analysis and calculation,it is found that the algorithm of the launcher servo control at large angle overflows because of its software and hardware design constraints,which might cause the seeker servo abnormal.After the software control algorithm of the launcher is compressed,the seeker servo is normal.The dynamic tests verify that the fault positioning is accurate,and the improved design method is effective,which meets the demand of large angle servo of the system. |
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| Keywords: | launcher large angle servo overflow |
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