Invention Grant
- Patent Title: Navigation satellite orbit and low latency clock determination with wide-lane and narrow-lane bias corrections
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Application No.: US15448466Application Date: 2017-03-02
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Publication No.: US10564293B2Publication Date: 2020-02-18
- Inventor: Yujie Zhang , Liwen L. Dai , Yiqun Chen
- Applicant: Deere & Company
- Applicant Address: US IL Moline
- Assignee: DEERE & COMPANY
- Current Assignee: DEERE & COMPANY
- Current Assignee Address: US IL Moline
- Agency: Morgan, Lewis & Bockius LLP
- Main IPC: G01S19/41
- IPC: G01S19/41 ; G01S19/07 ; G01S19/32 ; G01S19/44

Abstract:
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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