Differential positioning experiment using two geostationary satellites

被引：3
|
作者：
Ito, K [1 ]
Hoshinoo, K [1 ]
Ito, M [1 ]
机构：
[1] Elect Navigat Res Inst, Minist Transport, Mitaka, Tokyo 1810004, Japan
来源：
IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 1999年 / 35卷 / 03期
关键词：
D O I：
10.1109/7.784057
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A ranging and positioning system for a ship or an aircraft using two geostationary satellites is described. This system has a ranging and positioning accuracy of 100 m and 1 km. Experiments to estimate this system were performed using a ship in the Pacific Ocean in a normal and a differential modes. This system leads to the development of fundamental ranging and positioning techniques for the cooperated independent surveillance.
引用
收藏
页码：866 / 878
页数：13
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