| 惯导系统恒定工作温度的实现研究 |
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| 引用本文： | 柴卫华,何文昌,侯芸.惯导系统恒定工作温度的实现研究[J].现代防御技术,2001,29(5):46-49. |
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| 作者姓名： | 柴卫华 何文昌 侯芸 |
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| 作者单位： | 中国航天机电集团公司二院二部, |
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| 摘 要： | 介绍了一种实现惯导系统恒定工作温度的方法,并针对该系统的实际特点给出了该系统的硬件和软件组成,大量的实验结果表明该系统具有设计先进合理、可实现性强、可靠性高及可在诸多领域推广等特点.
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| 关 键 词： | 温度传感器(DS18B20) 惯性导航系统 单片机+(AT89C2051) |
| 文章编号： | 1009-086(2001)05-0046-04 |
| 修稿时间： | 2000年10月24 |
Study on the Temperature Stabilization of INS |
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| CHAI Wei hua,HE Wen chang,HOU Yun.Study on the Temperature Stabilization of INS[J].Modern Defence Technology,2001,29(5):46-49. |
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| Authors: | CHAI Wei hua HE Wen chang HOU Yun |
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| Abstract: | A method of realizing stable work temperature of INS is introduced, and according to the cha racteristic of the system, the configurations of hardware and software are given. Lots of experiments prove that the system design is advanced and reasonable, easy to realize, reliable and can be generalized for other applications. |
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| Keywords: | Temperature sensor (DS18B20) Inertial navigation system Single chip (AT89C2051) |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
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