发明名称 REAL-TIME AND POST-PROCESSED ORBIT DETERMINATION AND POSITIONING
摘要 Novel methods and systems for the accurate and efficient processing of real-time and latent global navigation satellite systems (GNSS) data are described. Such methods and systems can perform orbit determination of GNSS satellites, orbit determination of satellites carrying GNSS receivers, positioning of GNSS receivers, and environmental monitoring with GNSS data.
申请公布号 US2014316697(A1) 申请公布日期 2014.10.23
申请号 US201414256813 申请日期 2014.04.18
申请人 CALIFORNIA INSTITUTE OF TECHNOLOGY 发明人 BAR-SEVER Yoaz E.;BERTIGER William I.;DORSEY Angela R.;HARVEY Nathaniel E.;LU Wenwen;MILLER Kevin J.;MILLER Mark A.;ROMANS Larry J.;SIBTHORPE Anthony J.;WEISS Jan P.;FERNANDEZ Miquel Garcia;GROSS Jason
分类号 G01S19/13 主分类号 G01S19/13
代理机构 代理人
主权项 1. A method comprising: receiving, by a computer, measurements from at least one global navigation satellite system (GNSS) receiver; analyzing, by a computer, the measurements, thereby detecting and flagging anomalous measurements and phase breaks; calculating, by a computer, high-fidelity satellite and signal models that approximate the measurements, wherein the models comprise a plurality of model parameters having a priori values; estimating, by a computer, values for the plurality of model parameters affecting orbital and clock states of a GNSS satellite or affecting reception of said measurements by the at least one GNSS receiver, wherein the estimating is based on the measurements, thereby obtaining a plurality of estimated model parameters; calculating, by a computer, improved orbital and clock states based on the plurality of estimated model parameters and the measurements; calculating, by a computer, refined model parameters, additionally to the improved orbital and clock states, based on the plurality of estimated model parameters and the measurements; and transmitting, by a computer, the improved orbital and clock states and the refined model parameters to the at least one GNSS receiver.
地址 Pasadena CA US