Mobile reference station for GNSS positioning

Patent metadata

Field	Value
Publication number	US-11879982-B2
Application number	US-202117142951-A
Country	US
Kind code	B2
Filing date	Jan 6, 2021
Priority date	Jul 29, 2016
Publication date	Jan 23, 2024
Grant date	Jan 23, 2024

Abstract

Methods for determining corrected positions of a global navigation satellite system (GNSS) rover using a GNSS base station and one or more GNSS reference stations include determining a statistical representation of position measurements from the GNSS reference stations and an instantaneous position measurement from the GNSS reference stations. A position correction is determined based on the statistical representation and the instantaneous position measurement. A corrected position of the GNSS rover is determined based on a position of the GNSS rover and the position correction.

First claim

What is claimed is:

1. A method for determining corrected positions of a global navigation satellite system (GNSS) rover using a GNSS base station and a plurality of GNSS reference stations, the method comprising:
performing a first plurality of position measurements at a first GNSS reference station, the first GNSS reference station being one of the plurality of GNSS reference stations, the first GNSS reference station arranged at a first location while the first plurality of position measurements are determined, the first plurality of position measurements determined using corrections received from the GNSS base station and signals received at the first GNSS reference station from GNSS satellites, wherein the first plurality of position measurements are determined while the first GNSS reference station is stationary;
performing a second plurality of position measurements at a second GNSS reference station different from the first GNSS reference station, the second GNSS reference station being one of the plurality of GNSS reference stations, the second GNSS reference station arranged at a second location while the second plurality of position measurements are determined, the second plurality of position measurements determined using corrections received from the GNSS base station and signals received at the second GNSS reference station from GNSS satellites, wherein the second plurality of position measurements are determined while the second GNSS reference station is stationary;
determining a position of the GNSS rover using corrections received from the GNSS base station and signals received at the GNSS rover from GNSS satellites;
determining a position correction based on the first plurality of position measurements and the second plurality of position measurements;
determining a corrected position of the GNSS rover based on the position of the GNSS rover and the position correction.

2. The method of claim 1 wherein the position correction is a vertical correction that is determined based on a first difference between a statistical representation of the first plurality of position measurements and an instantaneous position of one of the first plurality of position measurements, and a second difference between a statistical representation of the second plurality of position measurements and an instantaneous position of one of the second plurality of position measurements.

3. The method of claim 1 wherein the corrections received from the GNSS base station are real-time kinematic (RTK) corrections.

4. The method of claim 1 wherein the first plurality of position measurements are determined one at a time and individually sent to the GNSS rover, the second plurality of position measurements are determined one at a time and individually sent to the GNSS rover, and the position correction and the corrected position are determined by the GNSS rover.

5. The method of claim 1 wherein the corrected position of the GNSS rover is also based on a scaling factor that is a function of a first distance between the GNSS rover and the first GNSS reference station, a second distance between the GNSS rover and the second GNSS reference station, and a third distance between the GNSS rover and the GNSS base station.

6. The method of claim 1 further comprising:
determining a third plurality of position measurements of a third GNSS reference station, the third GNSS reference station being one of the plurality of GNSS reference stations, the third GNSS reference station arranged at a third location while the third plurality of position measurements are determined, the third plurality of position measurements determined using corrections received from the GNSS base station and signals received at the third GNSS reference station from GNSS satellites, wherein the third plurality of position measurements are determined while the third GNSS reference station is stationary, and wherein the position correction is determined based on the first plurality of position measurements, the second plurality of position measurements, and the third plurality of position measurements.

7. The method of claim 1 wherein the position correction is determined based on a first vertical component of the first plurality of position measurements and a second vertical component of the second plurality of position measurements.

Assignees

• Trimble Inc

Inventors

• Cash Michael
• Riley Stuart
• Nadkarni Vivek

Classifications

• G01S19/40 Primary

  Correcting position, velocity or attitude · CPC title

• G01S19/07

  providing data for correcting measured positioning data, e.g. DGPS [differential GPS] or ionosphere corrections · CPC title

• G01S19/071 Primary

  DGPS corrections · CPC title

• G01S19/41

  Differential correction, e.g. DGPS [differential GPS] · CPC title

• G01S19/43

  using carrier phase measurements, e.g. kinematic positioning; using long or short baseline interferometry · CPC title