- 专利标题: Navigation satellite orbit and low latency clock determination with wide-lane and narrow-lane bias corrections
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申请号: US15448466申请日: 2017-03-02
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公开(公告)号: US10564293B2公开(公告)日: 2020-02-18
- 发明人: Yujie Zhang , Liwen L. Dai , Yiqun Chen
- 申请人: Deere & Company
- 申请人地址: US IL Moline
- 专利权人: DEERE & COMPANY
- 当前专利权人: DEERE & COMPANY
- 当前专利权人地址: US IL Moline
- 代理机构: Morgan, Lewis & Bockius LLP
- 主分类号: G01S19/41
- IPC分类号: G01S19/41 ; G01S19/07 ; G01S19/32 ; G01S19/44
摘要:
A satellite corrections generation system receives reference receiver measurement information from a plurality of reference receivers at established locations. In accordance with the received reference receiver measurement information, and established locations of the reference receivers, the system determines narrow-lane navigation solutions for the plurality of reference receivers. The system also determines clusters of single-difference (SD) narrow-lane floating ambiguities, each cluster comprising pairs of SD narrow-lane floating ambiguities for respective pairs of satellites. A satellite narrow-lane bias value for each satellite of a plurality of satellites is initially determined in accordance with fractional portions of the SD narrow-lane floating ambiguities in the clusters, and then periodically updated by a Kalman filter. A set of navigation satellite corrections for each satellite, including the satellite narrow-lane bias value for each satellite, is generated and transmitted to navigation receivers for use in determining locations of the navigation receivers.
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