Methods and apparatuses for multipath estimation and correction in GNSS navigation systems

• US 9,423,507 B2
• Filed: 05/30/2012
• Issued: 08/23/2016
• Est. Priority Date: 05/30/2012
• Status: Active Grant

• Current Assignee: CSR Technology Incorporated (Qualcomm, Inc.)
• Original Assignee: CSR Technology Incorporated (Qualcomm, Inc.)
• Inventors: Lin, Xiangdong, Tuck, David Allan, Chansarkar, Mangesh
• Primary Examiner(s): GALT, CASSI J
• Application Number:
  US13/484,217
• Publication Number:
  US 20130321202A1
• Time in Patent Office: 1,546 Days
• Field of Search: 342/357.61, 342/357.23
• US Class Current: 1/1
• CPC Class Codes: G01S 19/22 Multipath-related issues
• CPC Class Codes: G01S 19/40 Correcting position, velocity or attitude
• CPC Class Codes: G01S 19/428 using multipath or indirect path propagation signals in position determination

Abstract

The present invention relates generally to methods and apparatuses for estimating and correcting for multipath in GNSS navigation systems. According to some aspects, the invention operates in situations where position and estimated position error are reasonably stable so as to detect when large multipath errors are present with confidence. After detection, the slowly varying biases from multipath or other un-modeled sources can be modeled separately from the navigation state. The measurements are kept in the solution without biasing the navigation state thereby ignoring the long-term biases for use over short-term periods with minimized pseudorange error when necessary.

Claims

1. A method implemented by a receiver, comprising:

measuring, at the receiver, a signal from a satellite to obtain a pseudorange measurement;

determining whether a velocity of the receiver is less than a first threshold;

computing a pseudorange residual using the obtained pseudorange measurement in response to determining that the velocity of the receiver is less than the first threshold;

comparing the pseudorange residual to a second threshold to determine whether the pseudorange residual is less than a second threshold;

determining a pseudorange bias associated with the signal from a pseudorange bias model in response to determining that the pseudorange residual is not less than the second threshold;

removing the determined pseudorange bias from the pseudorange measurement;

updating a navigation state of the receiver using the pseudorange measurement, wherein the navigation state of the receiver is updated using the pseudorange measurement with the pseudorange bias removed in response to determining that the pseudorange residual is not less than the second threshold, and

the navigation state of the receiver is updated using the pseudorange measurement without the pseudorange bias removed in response to determining that at least one of the pseudorange residual is less than the second threshold and the velocity of the receiver is not less than the first threshold.

2. A method according to claim 1, wherein the receiver is a Global Navigation Satellite System (GNSS) receiver.

3. A method according to claim 1, wherein the pseudorange bias is due to a slowly varying condition.

4. A method according to claim 3, wherein the slowly varying condition is multipath.

5. A method according to claim 1, wherein computing the pseudorange residual includes determining an estimated pseudorange using ephemeris information for the satellite.

6. A receiver device comprising:

a GPS chipset; and

a processor configured with processor executable instructions to;

measure a signal from a satellite to obtain a pseudorange measurement;

determine whether a velocity of the receiver device is less than a first threshold;

compute a pseudorange residual using the obtained pseudorange measurement in response to determining that the velocity of the receiver device is less than the first threshold;

compare the pseudorange residual to a second threshold to determine whether the pseudorange residual is less than a second threshold;

determine a pseudorange bias associated with the signal from a pseudorange bias model in response to determining that the pseudorange residual is not less than the second threshold;

remove the determined pseudorange bias from the pseudorange measurement;

update a navigation state of the receiver device using the pseudorange measurement, wherein the navigation state of the receiver device is updated using the pseudorange measurement with the pseudorange bias removed in response to determining that the pseudorange residual is not less than the second threshold, and

the navigation state of the receiver device is updated using the pseudorange measurement without the pseudorange bias removed in response to determining that at least one of the pseudorange residual is less than the second threshold and the velocity of the receiver is not less than the first threshold.

7. A receiver device according to claim 6, wherein the receiver device is a Global Navigation Satellite System (GNSS) receiver.

8. A receiver device according to claim 6, wherein the pseudorange bias is due to a slowly varying condition.

9. A receiver device according to claim 8, wherein the slowly varying condition is multipath.

10. A receiver device according to claim 6, wherein the processor is further configured with processor executable instructions such that computing the pseudorange residual is performed by determining an estimated pseudorange using ephemeris information for the satellite.