| 基于固体燃气姿控舵机的自振荡阻尼回路设计 |
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| 引用本文： | 李遗.基于固体燃气姿控舵机的自振荡阻尼回路设计[J].弹箭与制导学报,2009,29(1). |
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| 作者姓名： | 李遗 |
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| 作者单位： | 北京理工大学宇航科学技术学院,北京,100081 |
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| 摘 要： | 为了描述自振荡阻尼回路的设计方法,以某小型战术导弹为例,设计了基于固体燃气姿控舵机的自振荡阻尼回路原理,详细描述了阻尼回路校正网络参数设计方法和设计过程,并对阻尼回路进行了仿真验证,结果表明参数设计正确,满足要求。
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| 关 键 词： | 燃气舵机 阻尼回路 自振荡 战术导弹 姿态控制 |
The Design of Self Sustained Oscillations Damping Loop Dased on Solid Gas Vane |
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| LI Yi.The Design of Self Sustained Oscillations Damping Loop Dased on Solid Gas Vane[J].Journal of Projectiles Rockets Missiles and Guidance,2009,29(1). |
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| Authors: | LI Yi |
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| Affiliation: | School of Aerospace Science and Engineering;Beijing Institute of Technology;Beijing 100081;China |
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| Abstract: | In order to describe the design method of the self sustained oscillations damping loop,the loop based on solid gas vane is designed,the design method and the design procedure of the correction parameter of the damping loop are described in detail,and the damping loop is emulated.The results indicate that the parameter design is perfect and meet the challenge. |
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| Keywords: | hot pneumatic actuator damping loop self sustained oscillations tactical missile attitude control |
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