Outlier-tolerant navigation satellite system positioning method and system

US10895646B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10895646-B2
Application numberUS-201715827664-A
CountryUS
Kind codeB2
Filing dateNov 30, 2017
Priority dateDec 19, 2016
Publication dateJan 19, 2021
Grant dateJan 19, 2021

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

The invention relates to a method carried out by a navigation satellite system (NSS) receiver or a processing entity receiving data therefrom, for estimating parameters useful to determine a position. The NSS receiver observes NSS signals from NSS satellites. Two filters, called “robustifier” and “main estimator” respectively, both use state variables and compute the values thereof based on: NSS signals observed by the NSS receiver, and/or information derived therefrom. The robustifier identifies, within the input data, measurements that do not match a stochastic model assigned thereto. For each identified measurement, the robustifier rejects the measurement, adjusts the stochastic model assigned to the measurement, and/or corrects the measurement. The robustifier uses fewer state variables than the main estimator. A corresponding system is also disclosed.

First claim

Opening claim text (preview).

The invention claimed is: 1. Method, carried out by at least one of a navigation satellite system receiver, hereinafter abbreviated as “NSS receiver”, and a processing entity capable of receiving data from the NSS receiver, for estimating parameters useful to determine a position, the NSS receiver observing a NSS signal from each of a plurality of NSS satellites over multiple epochs, the method comprising: receiving input data comprising at least one of: NSS signals observed by the NSS receiver, and information derived from said NSS signals; and operating a first filter, hereinafter referred to as “robustifier”, and a second filter, hereinafter referred to as “main estimator”, wherein: each of the robustifier and main estimator uses state variables, and computes the values of their respective state variables at least based on the received input data; the robustifier identifies, within the received input data, any measurement that does not match a stochastic model assigned thereto; for each measurement identified by the robustifier as not matching its stochastic model, at least one of the following applies: the robustifier rejects the measurement, and the main estimator does not use the rejected measurement; the robustifier adjusts the stochastic model assigned to the measurement, and the main estimator uses the adjusted stochastic model; and the robustifier corrects the measurement, and the main estimator uses the corrected measurement; and the robustifier uses fewer state variables than the main estimator. 2. Method of claim 1 , wherein the main estimator comprises at least one of a Kalman filter, and a least squares estimator. 3. Method of claim 1 , wherein the robustifier comprises at least one of: an M-estimator, a BIBER estimator, a least median squares (LMS) estimator, a least trimmed squares (LTS) estimator, an S-estimator, and an L1 estimator. 4. Method according to claim 1 , wherein the robustifier uses at least the following state variables: three state variables representing at least one of: the position of the NSS receiver, an offset in the position of the NSS receiver relative to another position, and a change in the position of the NSS receiver; and a state variable representing at least one of: a NSS common bias term for at least one NSS, an offset in said NSS common bias term relative to another NSS common bias term, and a change in a NSS common bias. 5. Method of claim 4 , wherein the robustifier uses only: said three state variables representing at least one of: the position of the NSS receiver, an offset in the position of the NSS receiver relative to another position, and a change in the position of the NSS receiver; and said state variable representing at least one of: the NSS common bias term for at least one NSS, an offset in said NSS common bias term relative to another NSS common bias term, and a change in a NSS common bias. 6. Method according to claim 1 , wherein each of the multiple epochs over which the NSS receiver observes a NSS signal from each of a plurality of NSS satellites is hereinafter referred to as “receiver epoch”, and, at each receiver epoch, the robustifier identifies, within the received input data, any measurement that does not match the stochastic model assigned thereto, and for each measurement identified as not matching its stochastic model, performs at least one of the following operations: rejecting the measurement, adjusting the stochastic model assigned to the measurement, and correcting the measurement. 7. Method according to claim 1 , wherein the received input data is corrected for systematic errors before the robustifier uses said received input data. 8. Method according to claim 1 , wherein measurements comprised in the received input data are assigned their stochastic model before the robustifier uses said received input data. 9. Method according to claim 1 , wherein the robustifier further receives, from the main estimator, values of state variables used by the main estimator; identifies an error within the received values; and provides feedback thereon to the main estimator. 10. System comprising at least one of a navigation satellite system receiver, hereinafter abbreviated as “NSS receiver”, and a processing entity capable of receiving data from the NSS receiver, for estimating parameters useful to determine a position, the NSS receiver being configured to observe a NSS signal from each of a plurality of NSS satellites over multiple epochs, the system being configured for receiving input data comprising at least one of: NSS signals observed by the NSS receiver, and information derived from said NSS signals; and the system is configured to operate a first filter, hereinafter referred to as “robustifier”, and a second filter, hereinafter referred to as “main estimator”, wherein the robustifier and the main estimator are configured so that, in operation: each of the robustifier and main estimator uses state variables, and computes the values of their respective state variables at least based on the received input data; the robustifier identifies, within the received input data, any measurement that does not match a stochastic model assigned thereto; for each measurement identified by the robustifier as not matching its stochastic model, at least one of the following applies: the robustifier rejects the measurement, and the main estimator does not use the rejected measurement; the robustifier adjusts the stochastic model assigned to the measurement, and the main estimator uses the adjusted stochastic model; and the robustifier corrects the measurement, and the main estimator uses the corrected measurement; and the robustifier uses fewer state variables than the main estimator. 11. System of claim 10 , wherein the main estimator comprises at least one of a Kalman filter, and a least squares estimator. 12. System of claim 10 , wherein the robustifier comprises at least one of: an M-estimator, a BIBER estimator, a least median squares (LMS) estimator, a least trimmed squares (LTS) estimator, an S-estimator, and an L1 estimator. 13. System according to claim 10 , wherein the robustifier is configured so that, in operation, it uses at least the following state variables: three state variables representing at least one of: the position of the NSS receiver, an offset in the position of the NSS receiver relative to another position, and a change in the position of the NSS receiver; and a state variable representing at least one of: a NSS common bias term for at least one NSS, an offset in said NSS common bias term relative to another NSS common bias term, and a change in a NSS common bias. 14. System of claim 13 , wherein the robustifier is configured so that, in operation, it uses only: said three state variables representing at least one of: the position of the NSS receiver, an offset in the position of the NSS receiver relative to another position, and a change in the position of the NSS receiver; and said state variable representing at least one of: the NSS common bias term for at least one NSS, an offset in said NSS common bias term relative to another NSS common bias term, and a change in a NSS common bias. 15. System according to claim 10 , wherein each of the multiple epochs over which the NSS receiver is configured to observe a NSS signal from each of a plurality of NSS satellites is hereinafter referred to as “receiver epoch”, and, the robustifier is configured so that, at each receiver epoch, it identifies, within the

Assignees

Inventors

Classifications

  • G01S19/42Primary

    Determining position · CPC title

  • G01S19/29Primary

    carrier {including Doppler,} related {(G01S19/246 takes precedence)} · CPC title

  • Correcting position, velocity or attitude · CPC title

  • Carrier phase ambiguity resolution; Floating ambiguity; LAMBDA [Least-squares AMBiguity Decorrelation Adjustment] method · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US10895646B2 cover?
The invention relates to a method carried out by a navigation satellite system (NSS) receiver or a processing entity receiving data therefrom, for estimating parameters useful to determine a position. The NSS receiver observes NSS signals from NSS satellites. Two filters, called “robustifier” and “main estimator” respectively, both use state variables and compute the values thereof based on: NS…
Who is the assignee on this patent?
Trimble Inc
What technology area does this patent fall under?
Primary CPC classification G01S19/42. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Jan 19 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).