Recovery of high precision position after GNSS outage

Patent metadata

Field	Value
Publication number	US-11221417-B2
Application number	US-201916298948-A
Country	US
Kind code	B2
Filing date	Mar 11, 2019
Priority date	Dec 27, 2018
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

A system and method for estimating a position. In some embodiments, the method includes receiving global navigation satellite system signals from a plurality of global navigation satellite system satellites; receiving a plurality of reference station measurements; receiving external error correction data; generating first position estimates with a Real-Time Kinematic method, based on the global navigation satellite system signals and on the reference station measurements; and generating second position estimates with a Precise Point Positioning method, based on the global navigation satellite system signals, on the external error correction data, and on first position estimates.

First claim

What is claimed is:

1. A method for estimating a position of a global navigation satellite system receiver, the method comprising:
operating in a first state;
determining that a state transition criterion is met; and
in response to determining that the state transition criterion is met, operating in a second state;
the operating in the first state comprising:
receiving global navigation satellite system signals from a plurality of global navigation satellite system satellites;
receiving a plurality of reference station measurements;
receiving external error correction data;
generating first position estimates with a Real-Time Kinematic method, based on the global navigation satellite system signals and on the reference station measurements; and
generating second position estimates with a Precise Point Positioning method, based on the global navigation satellite system signals, on the external error correction data, and on the first position estimates;

the determining that the state transition criterion is met comprising determining that a measure of convergence of the Precise Point Positioning method meets a convergence criterion, wherein the measure of convergence is an estimated covariance of an extended Kalman filter of the Precise Point Positioning method and the convergence criterion is met when a magnitude of the estimated covariance is below a threshold; and
the operating in the second state comprising:
receiving global navigation satellite system signals from a plurality of global navigation satellite system satellites,
receiving external error correction data; and
generating the second position estimates with a Precise Point Positioning method, based on the global navigation satellite system signals, and on the external error correction data.

2. The method of claim 1 , wherein the receiving of a plurality of reference station measurements comprises receiving a plurality of reference station measurements from a non-physical reference station.

3. The method of claim 1 , further comprising operating in a third state before operating in the first state, the operating in the third state comprising not receiving global navigation satellite system signals from a plurality of global navigation satellite system satellites.

4. The method of claim 3 , further comprising operating in a fourth state before operating in the third state, the measure of convergence of the Precise Point Positioning method meeting the convergence criterion while operating in the fourth state.

5. The method of claim 4 , wherein an interval of time between the operating in the fourth state and the operating in the first state is less than four minutes.

6. The method of claim 1 , wherein the generating of the first position estimates comprises utilizing ionosphere-free combination.

7. The method of claim 1 , wherein the generating of the first position estimates comprises utilizing cascading ambiguity resolution.

8. The method of claim 1 , wherein the receiving of global navigation satellite system signals from a plurality of global navigation satellite system satellites comprises receiving global navigation satellite system signals from a Global Positioning System satellite.

9. The method of claim 1 , wherein the receiving of global navigation satellite system signals from a plurality of global navigation satellite system satellites comprises:
receiving an L1 signal from a Global Positioning System satellite, and
receiving an L2 signal from a Global Positioning System satellite.

10. A system for estimating a position of a global navigation satellite system receiver, the system comprising:
a first receiving circuit, for receiving global navigation satellite system signals; and
a second receiving circuit, for receiving reference signals; and
a processing circuit,
the system being configured to:
operate in a first state;
determine that a state transition criterion is met; and
in response to determining that the state transition criterion is met, operate in a second state;

the operating in the first state comprising:
receiving, by the first receiving circuit, global navigation satellite system signals from a plurality of global navigation satellite system satellites;
receiving, by the second receiving circuit, a plurality of reference station measurements;
receiving, by the second receiving circuit, external error correction data;
generating, by the processing circuit, first position estimates with a Real-Time Kinematic method, based on the global navigation satellite system signals and on the reference station measurements; and
generating, by the processing circuit, second position estimates with a Precise Point Positioning method, based on the global navigation satellite system signals, on the external error correction data, and on first position estimates;

the determining that the state transition criterion is met comprising determining, by the processing circuit, that a measure of convergence of the Precise Point Positioning method meets a convergence criterion, wherein the measure of convergence is an estimated covariance of an extended Kalman filter of the Precise Point Positioning method and the convergence criterion is met when a magnitude of the estimated covariance is below a threshold; and
the operating in the second state comprising:
receiving, by the first receiving circuit, global navigation satellite system signals from a plurality of global navigation satellite system satellites,
receiving, by the second receiving circuit, external error correction data; and
generating, by the processing circuit, the second position estimates with a Precise Point Positioning method, based on the global navigation satellite system signals, and on the external error correction data.

11. The system of claim 10 , wherein the receiving of a plurality of reference station measurements comprises receiving a plurality of reference station measurements from a non-physical reference station.

12. The system of claim 10 , further configured to operate in a third state before operating in the first state, the operating in the third state comprising not receiving global navigation satellite system signals from a plurality of global navigation satellite system satellites.

13. The system of claim 12 , further configured to operate in a fourth state before operating in the third state, the measure of convergence of the Precise Point Positioning method meeting the convergence criterion while operating in the fourth state.

14. The system of claim 13 , wherein an interval of time between the operating in the fourth state and the operating the first state is less than four minutes.

15. The system of claim 10 , wherein the generating of the first position estimates comprises utilizing ionosphere-free combination.

16. The system of claim 10 , wherein the generating of the first position estimates comprises utilizing cascading ambiguity resolution.

17. The system of claim 10 , wherein the receiving of global navigation satellite system signals from a plurality of global navigation satellite system satellites comprises receiving global navigation satellite system signals from a Global Positioning System satellite.

18. A system for estimating a position of a global navigation satellite system receiver, the system comprising:
first receiving means, for receiving global navigation satellite system signals; and
second receiving means, for receiving terrestrial signals; and
processing means,
the system being configured to:
operate in a first state;
determine that

Assignees

• Samsung Electronics Co Ltd

Inventors

• Zhang Wentao

Classifications

• G01S19/43

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

• G01S19/10 Primary

  providing dedicated supplementary positioning signals · CPC title

• G01S19/32

  Multimode operation in a single same satellite system, e.g. GPS L1/L2 · CPC title

• G01S19/07

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

• G01S19/40 Primary

  Correcting position, velocity or attitude · CPC title