发明名称 ABSOLUTE POSITION DETERMINATION METHOD IN SATELLITE NAVIGATION SYSTEM AND SATELLITE NAVIGATION SYSTEM
摘要 PROBLEM TO BE SOLVED: To attain a highly precise positioning by precisely defining absolute positions of navigation satellites. SOLUTION: As for the respective navigation satellites, distances between respective interesting navigation satellites and at least three navigation satellites other than the interesting one are measured by an inter-satellite communication range finding. At least six sets of proper measurements between at least three control stations and at least the three navigation satellites are performed. Absolute positions of respective navigation satellites referring to the globe as standards are introduced based on measured inter satellite distances, between ground and satellite distances, and absolute positions of the control stations. COPYRIGHT: (C)2004,JPO&NCIPI
申请公布号 JP2004251778(A) 申请公布日期 2004.09.09
申请号 JP20030042947 申请日期 2003.02.20
申请人 NATL SPACE DEVELOPMENT AGENCY OF JAPAN 发明人 INAMIYA KENICHI
分类号 B64G3/00;G01S19/02;(IPC1-7):G01S5/14 主分类号 B64G3/00
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