Research on integrated navigation systemby rubidium clock
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Research on integrated navigation systemby rubidium clock
Issue 8, Pages: 144-147(2006)
作者机构:
1. 海军航空工程学院电子信息工程系
2. 海军航空工程学院电子信息工程系,山东,烟台,264001
作者简介:
基金信息:
DOI:
CLC:P228.4
Published:2006
稿件说明:
移动端阅览
LI Ting-jun, LIN Xue-yuan, DONG Wen-hong, et al. Research on integrated navigation systemby rubidium clock[J]. 2006, (8): 144-147.
DOI:
LI Ting-jun, LIN Xue-yuan, DONG Wen-hong, et al. Research on integrated navigation systemby rubidium clock[J]. 2006, (8): 144-147.DOI:
Research on integrated navigation systemby rubidium clock
摘要
介绍了双星定位系统(RDSS)的局限性
提出了利用高精度时钟
即铷钟作为接收机内部时钟
如接收机能够测量用户至卫星的伪距
在气压高度表的辅助下
双星定位系统可以与捷联惯导进行有效的伪距组合。仿真结果表明
组合后的导航系统具有输出导航参数误差小的特点
为发展双星定位系统提出了一条新的思路。
Abstract
On the basis of introducing the limitations of the double-star positioning system
the precision rubidium clock was put forward to be the internal clock of the RDSS receiver.If the receiver could measure the pseudo-ranges from the user to the satellites
with the help of barometer
the RDSS could be integrated with the strap-down inertial navigation system based on pseudo-range.The simulation result shows that the output navigation parameters of the integrated sys-tem have the characteristic of low error
which offers one new way to develop our country’s RDSS.