| 无陀螺捷联惯导系统 |
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| 引用本文： | 马澍田,陈世有,李艳梅,张海霞.无陀螺捷联惯导系统[J].航空学报,1997,18(4):484-488. |
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| 作者姓名： | 马澍田 陈世有 李艳梅 张海霞 |
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| 作者单位： | 哈尔滨工程大学 |
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| 摘 要： | 阐述了无陀螺捷联惯导系统的原理，推导了其力学编排方程，提出并论证了提高载体角速度的计算值精度的方法。从而得到了适于工程应用的无陀螺捷联惯导系统方案，对该方案进行了计算机仿真计算。得到了满意的结果。
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| 关 键 词： | 导航 惯性导航 捷联惯导 无陀螺 |
| 收稿时间： | 1996-08-06; |
| 修稿时间： | 1997-01-20 |
NONGYROSCOPIC STRAPDOWN INERTIAL NAVIGATION SYSTEM |
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| Ma Shutian,Chen Shiyou,Li Yanmei,Zhang Haixia.NONGYROSCOPIC STRAPDOWN INERTIAL NAVIGATION SYSTEM[J].Acta Aeronautica et Astronautica Sinica,1997,18(4):484-488. |
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| Authors: | Ma Shutian Chen Shiyou Li Yanmei Zhang Haixia |
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| Institution: | Harbin Engineering Institute, Harbin, 150001 |
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| Abstract: | The principle of the nongyroscopic strapdown inertial navigation system is discussed. The mechanical calibration equations are formulated, and the methods to improve the accuracy of the calculation of the carrier's angular velocity are proposed and analyzed. Then the configuration which is practical to the engineering application is obtained. The configuration is simulated on the computer, and the results are satisfying |
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| Keywords: | navigation inertial navigation strapdown nongyroscopic |
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