首页> 外文会议>Saint Petersburg International Conference on Integrated Navigation Systems; 20030526-28; St.Petersburg(RU) >DEVELOPMENT AND TEST RESULTS FOR A SMALL-SIZE INERTIAL NAVIGATION SYSTEM BASED ON DYNAMICALLY TUNED GYROS
【24h】

DEVELOPMENT AND TEST RESULTS FOR A SMALL-SIZE INERTIAL NAVIGATION SYSTEM BASED ON DYNAMICALLY TUNED GYROS

机译:基于动力陀螺仪的小型惯性导航系统的研制与试验结果

获取原文
获取原文并翻译 | 示例

摘要

This paper presents the results of the ground and sea trials of a small-size menial navigation system (INS) based on dynamically tuned gyros (DTG). It is shown that the use of DTG based on a ball bearing support allows to realize DTG of inertial class and INS based on it. The aim of this paper is to present the results of the development and test of a small-size inertial navigation system with short readiness time, based on dynamically tuned gyros.
机译:本文介绍了基于动态调谐陀螺仪(DTG)的小型卫星导航系统(INS)的地面和海上试验结果。结果表明,基于滚珠轴承支撑的DTG的使用可以实现惯性级的DTG和基于它的INS。本文的目的是介绍基于动态调谐陀螺仪的,准备时间短的小型惯性导航系统的开发和测试结果。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号