Navigation satellite system positioning with enhanced satellite-specific correction information

US10018728B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10018728-B2
Application numberUS-201414569194-A
CountryUS
Kind codeB2
Filing dateDec 12, 2014
Priority dateDec 17, 2013
Publication dateJul 10, 2018
Grant dateJul 10, 2018

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 methods, notably carried out by global or regional navigation satellite system (NSS) receivers, which involve receiving satellite-specific, nadir-angle dependent correction information associated with each of at least two NSS satellites among a plurality of NSS satellites. The correction information is useful to correct observed NSS signals, so as to mitigate the effects of satellite-specific, nadir-angle dependent biases in the NSS signals, and thus improve the performance of position determination systems. The invention also relates to methods for generating such correction information, to methods for designing a satellite, to NSS receivers, to apparatuses for generating correction information to be sent to the receivers, and to computer programs and storage mediums.

First claim

Opening claim text (preview).

The invention claimed is: 1. Method, carried out by a global or regional navigation satellite system receiver, hereinafter abbreviated as NSS receiver, or by a NSS receiver and a processing entity connected to the NSS receiver, to estimate parameters derived at least from NSS signals, the method comprising: observing a NSS signal from each of a plurality of NSS satellites; receiving “satellite-specific-nadir-angle-dependent-correction-information” associated with each of at least two NSS satellites among the plurality of NSS satellites, wherein generating the satellite-specific-nadir-angle-dependent-correction-information includes: receiving raw observations obtained by observing NSS signals from each of the at least two NSS satellites from a plurality of reference stations; determining combination values based on the raw observations to cancel out effects of clocks, effects of troposphere, and effects of ionosphere; and generating the satellite-specific-nadir-angle-dependent-correction-information based on a difference between the determined combination values and a satellite specific reference value that is constant over all nadir angles; wherein the satellite-specific-nadir-angle-dependent-correction-information associated with each of the at least two NSS satellites comprises satellite-specific pseudorange correction information that depends on a nadir angle of the NSS receiver as seen from the NSS satellite; processing the observed NSS signals from the plurality of NSS satellites using the satellite-specific-nadir-angle-dependent-correction-information to correct the observed NSS signals or data derived therefrom so as to mitigate the effects of satellite-specific, nadir-angle dependent pseudorange biases in the NSS signals from the NSS satellites; estimating the parameters based at least in part on the processed NSS signals; and determining the position of the NSS receiver based at least in part on the parameters. 2. Method of claim 1 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises frequency-specific correction information. 3. Method of claim 1 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with each of the plurality of NSS satellites. 4. Method of claim 1 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with at least one BeiDou satellite. 5. Method of claim 4 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with a majority of the BeiDou satellites. 6. Method of claim 5 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with the entire constellation of BeiDou satellites. 7. Method of claim 1 , wherein the method uses carrier phase and pseudorange measurements of the NSS signals. 8. A non-transitory computer readable medium comprising computer-executable instructions configured, when executed on a computer, to carry out a method according to claim 1 . 9. Navigation satellite system (NSS) receiver for estimating parameters derived at least from NSS signals, the NSS receiver comprising: a first unit, hereinafter referred to as “first receiving unit”, configured for observing a NSS signal from each of a plurality of NSS satellites; a second unit, hereinafter referred to as “second receiving unit”, configured for receiving “satellite-specific-nadir-angle-dependent-correction-information” associated with each of at least two NSS satellites among the plurality of NSS satellites, wherein the satellite-specific-nadir-angle-dependent-correction-information is generated from: raw observations obtained by observing NSS signals from each of the at least two NSS satellites from a plurality of reference stations; and combination values based on the raw observations, the combination values canceling out effects of clocks, effects of troposphere, and effects of ionosphere; wherein the satellite-specific-nadir-angle-dependent-correction-information is based on a difference between the combination values and a satellite specific reference value that is constant over all nadir angles, and the satellite-specific-nadir-angle-dependent-correction-information associated with each of the at least two NSS satellites comprises satellite-specific pseudorange correction information that depends on a nadir angle of the NSS receiver as seen from the NSS satellite; and a third unit, hereinafter referred to as “processing unit”, configured for processing the observed NSS signals from the plurality of NSS satellites using the satellite-specific-nadir-angle-dependent-correction-information to correct the observed NSS signals or data derived therefrom so as to mitigate the effects of satellite-specific, nadir-angle dependent pseudorange biases in the NSS signals from the NSS satellites, the processing unit also configured for estimating the parameters based at least in part on the processed NSS signals and for determining the position of the NSS receiver based at least in part on the parameters. 10. NSS receiver of claim 9 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises frequency-specific correction information. 11. NSS receiver of claim 9 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with each of the plurality of NSS satellites. 12. NSS receiver of claim 9 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with at least one BeiDou satellite. 13. NSS receiver of claim 12 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with a majority of the BeiDou satellites. 14. NSS receiver of claim 13 , wherein the satellite-specific-nadir-angle-dependent-correction-information associated with the at least two NSS satellites comprises satellite-specific-nadir-angle-dependent-correction-information associated with the entire constellation of BeiDou satellites. 15. NSS receiver of claim 9 , wherein the NSS receiver is configured to use carrier phase and pseudorange measurements of the NSS signals.

Assignees

Inventors

Classifications

  • involving a network of fixed stations · CPC title

  • G01S19/072Primary

    Ionosphere corrections · CPC title

  • Determining position · CPC title

  • providing carrier phase data · CPC title

  • G01S19/13Primary

    Receivers · 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 US10018728B2 cover?
The invention relates to methods, notably carried out by global or regional navigation satellite system (NSS) receivers, which involve receiving satellite-specific, nadir-angle dependent correction information associated with each of at least two NSS satellites among a plurality of NSS satellites. The correction information is useful to correct observed NSS signals, so as to mitigate the effect…
Who is the assignee on this patent?
Trimble Inc
What technology area does this patent fall under?
Primary CPC classification G01S19/072. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Jul 10 2018 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).