| 激光陀螺在中、远程防空导弹上的应用 |
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| 引用本文： | 赵冰,梁明,刘鑫.激光陀螺在中、远程防空导弹上的应用[J].上海航天,2002,19(4):51-53. |
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| 作者姓名： | 赵冰 梁明 刘鑫 |
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| 作者单位： | 中国人民解放军92941部队,辽宁,葫芦岛,125001 |
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| 摘 要： | 分析了激光陀螺的工作原理，介绍了激光陀螺的性能特点，提出激光陀螺具有传统的机电陀螺和其他类型陀螺所无法比拟的优点，其性能特征完全满足捷联惯导对惯性测量元件的要求，军事应用前景十分广阔，同时，对激光陀螺在新一代防空导弹上的应用作了展望。
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| 关 键 词： | 激光陀螺 标度因数 捷联惯性导航 |
| 文章编号： | 1006-1630(2002)04-0051-03 |
| 修稿时间： | 2002年1月11日 |
Application of Laser Gyro in the Medium and Long-Range Anti-Air Missile |
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| ZHAO Bing,LIANG Ming,LIU Xin.Application of Laser Gyro in the Medium and Long-Range Anti-Air Missile[J].Aerospace Shanghai,2002,19(4):51-53. |
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| Authors: | ZHAO Bing LIANG Ming LIU Xin |
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| Abstract: | The principle and features of the laser gyro are summarized in this paper. It is presented that laser gyro has predominant advantages over electric-mechanical and other types of gyros. It meets the demands of strap-down navigation system to inertia measure equipment and has a very strong application in military affairs. The expectation for the application in new generation of air defense missile is given. |
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| Keywords: | Laser gyro Air defense missile Strap-down inertia navigation system Calibration factor |
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