发明名称 System using leo satellites for centimeter-level navigation
摘要 Disclosed herein is a system for rapidly resolving position with centimeter-level accuracy for a mobile or stationary receiver [4]. This is achieved by estimating a set of parameters that are related to the integer cycle ambiguities which arise in tracking the carrier phase of satellite downlinks [5,6]. In the preferred embodiment, the technique involves a navigation receiver [4] simultaneously tracking transmissions [6] from Low Earth Orbit Satellites (LEOS) [2] together with transmissions [5] from GPS navigation satellites [1]. The rapid change in the line-of-sight vectors from the receiver [4] to the LEO signal sources [2], due to the orbital motion of the LEOS, enables the resolution with integrity of the integer cycle ambiguities of the GPS signals [5] as well as parameters related to the integer cycle ambiguity on the LEOS signals [6]. These parameters, once identified, enable real-time centimeter-level positioning of the receiver [4]. In order to achieve high-precision position estimates without the use of specialized electronics such as atomic clocks, the technique accounts for instabilities in the crystal oscillators driving the satellite transmitters, as well as those in the reference [3] and user [4] receivers. In addition, the algorithm accommodates as well as to LEOS that receive signals from ground-based transmitters, then re-transmit frequency-converted signals to the ground.
申请公布号 US6373432(B1) 申请公布日期 2002.04.16
申请号 US20000625419 申请日期 2000.07.25
申请人 THE BOARD OF TRUSTEES OF THE LELAND STANFORD JUNIOR UNIVERSITY 发明人 RABINOWITZ MATTHEW;PARKINSON BRADFORD W.;COHEN CLARK E.;LAWRENCE DAVID G.
分类号 G01C21/00;G01S5/14;G01S19/05;G01S19/11;G01S19/21;G01S19/29;G01S19/46;H04B7/185;(IPC1-7):G01S5/02 主分类号 G01C21/00
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