| 导引头火箭橇试验振动力学环境控制技术研究 |
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| 引用本文： | 解珍珍,陈诚,付良,谢波涛.导引头火箭橇试验振动力学环境控制技术研究[J].导航与控制,2015(6):27-31. |
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| 作者姓名： | 解珍珍 陈诚 付良 谢波涛 |
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| 作者单位： | 中国兵器工业试验测试研究院;中国兵器工业试验测试研究院;中国兵器工业试验测试研究院;中国兵器工业试验测试研究院 |
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| 摘 要： | 针对导引头系统的特点， 从火箭橇试验系统的振动源分析， 开展导引头系
统火箭橇试验的振动力学环境控制技术分析，通过对火箭橇体结构的气动优化设计及聚
氨酯泡沫填充剂的吸振作用和硅橡胶的减振作用的组合方式相结合降低导引头系统振动
环境，并利用仿真分析和火箭橇试验验证力学环境控制系统设计的合理性。
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| 关 键 词： | 导引头 火箭橇 力学控制 振动 |
Study on Control Technology of Mechanical Vibration
Environmental of Seeker Rocket Sled Test |
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| XIE Zhen-zhen,CHEN Cheng,FU Liang and XIE Bo-tao.Study on Control Technology of Mechanical Vibration
Environmental of Seeker Rocket Sled Test[J].Navigation and Control,2015(6):27-31. |
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| Authors: | XIE Zhen-zhen CHEN Cheng FU Liang and XIE Bo-tao |
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| Institution: | Norinco Group Test and Measuring Academy;Norinco Group Test and Measuring Academy;Norinco Group Test and Measuring Academy;Norinco Group Test and Measuring Academy |
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| Abstract: | Aiming at the characteristics of seeker system, analyzed from the vibration source of the rocket sled test
system. Carry out control technical analysis of mechanical vibration environmental of seeker system rocket sled test, and
reduce the combination of seeker system vibration environment by aerodynamic optimization of rocket sled structure and
polyurethane foam filling agent of reducing vibration and vibration absorption and silicone rubber combinations. Verifies
the rationality of the design of control system of mechanical environment by simulation analysis and rocket sled test. |
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| Keywords: | seeker rocket sled mechanical control vibration |
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