发明名称 SATELLITE POSITIONING SYSTEM, AND NAVIGATION SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide "a satellite positioning system and a navigation system" capable of restraining a position skip of a positioning position in satellite positioning. SOLUTION: When a great difference exceeding a threshold value Thd exists in a distance LS between a position P1 found by the satellite positioning based on a propagation lag of a received radio wave from a GPS satellite, by a GPS receiver 4, in a time T=1, and a position P0 found by the satellite positioning by a GPS receiver 4, in a time T=0 therebefore, this time positioning position is found finally based on a velocity vector V0 found based on a Doppler shift generated in the received radio wave from the GPS satellite, by the GPS receiver 4, in the time T=0 using the satellite positioning position as the positioning position, and based on the last positioning position, in positioning (T=1, 2) during the first period hereafter. This time positioning position is found based on a velocity vector V found by the GPS receiver 4 in a corresponding time and the last positioning position, in positioning (T=3, 4) during the second period thereafter. Processing is restored to one using the satellite positioning position as the positioning position, in positioning (T=5, 6) thereafter. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2005300167(A) 申请公布日期 2005.10.27
申请号 JP20040111930 申请日期 2004.04.06
申请人 ALPINE ELECTRONICS INC 发明人 WAKAMATSU KOTARO
分类号 G09B29/00;G01C21/00;G01C21/26;G01S19/28;G01S19/42;G01S19/50;G08G1/0969;G09B29/10;(IPC1-7):G01S5/14;G08G1/096 主分类号 G09B29/00
代理机构 代理人
主权项
地址