航空学报 > 1997, Vol. 18 Issue (4): 484-488

无陀螺捷联惯导系统

马澍田, 陈世有, 李艳梅, 张海霞   

  1. 哈尔滨工程大学
  • 收稿日期:1996-08-06 修回日期:1997-01-20 出版日期:1997-08-25 发布日期:1997-08-25

NONGYROSCOPIC STRAPDOWN INERTIAL NAVIGATION SYSTEM

Ma Shutian, Chen Shiyou, Li Yanmei, Zhang Haixia   

  1. Harbin Engineering Institute, Harbin, 150001
  • Received:1996-08-06 Revised:1997-01-20 Online:1997-08-25 Published:1997-08-25

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。

关键词: 导航, 惯性导航, 捷联惯导, 无陀螺

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

Key words: navigation, inertial navigation, strapdown, nongyroscopic

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