发明名称 SATELLITE POSITIONING METHOD AND SATELLITE POSITIONING SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a satellite positioning method which enables to find an own position, even in case of an attenuated satellite received signal, with ultra-sensitivity and good responsiveness, and enables to process the data in real time by reducing the amount of data stored for calculation. SOLUTION: In this satellite positioning method, a receiver terminal receives a signal from a satellite and calculates its position. Time equivalent to one bit of navigation data of the satellite received signal is divided in two periods at data acquisition start time: acquisition time T<SB>1</SB>which is the first half, and processing time T<SB>2</SB>which is the second half. Signals received during the acquisition time T<SB>1</SB>are processed by correlation calculation during the processing time T<SB>2</SB>. In addition, the predetermined number of received signals corresponding to the acquisition time T<SB>1</SB>is obtained by delaying the data acquisition start time by minute time i, and each of the received signals is also processed by correlation calculation during the processing time T<SB>2</SB>. COPYRIGHT: (C)2006,JPO&NCIPI
申请公布号 JP2005321298(A) 申请公布日期 2005.11.17
申请号 JP20040139614 申请日期 2004.05.10
申请人 MAZERAN SYSTEMS JAPAN KK 发明人 HIRATA SEIICHIRO;KISHIMOTO NOBUHIRO
分类号 G01S19/37;(IPC1-7):G01S5/14 主分类号 G01S19/37
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