Navigation satellite system positioning with enhanced satellite-specific correction information

Patent metadata

Field	Value
Publication number	US-10816670-B2
Application number	US-201815985196-A
Country	US
Kind code	B2
Filing date	May 21, 2018
Priority date	Dec 17, 2013
Publication date	Oct 27, 2020
Grant date	Oct 27, 2020

Abstract

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

The invention claimed is:

1. Method for generating correction information for use by a global or regional navigation satellite system receiver, hereinafter abbreviated as NSS receiver, to determine a position of the NSS receiver, the correction information hereinafter referred to as “satellite-specific-nadir-angle-dependent-correction-information”, the satellite-specific-nadir-angle-dependent-correction-information associated with each of at least two navigation satellite system (NSS) satellites among a plurality of NSS satellites, wherein the satellite-specific-nadir-angle-dependent-correction-information associated with a NSS satellite comprises correction information depending on the nadir angle of a receiver as seen from the NSS satellite, so as to mitigate effects of satellite-specific, nadir-angle dependent biases in the NSS signals from the NSS satellite, the method comprising, for each NSS satellite among the at least two NSS satellites:
receiving raw observations obtained by observing NSS signals from the NSS satellite from a plurality of reference stations;
computing combination values based on the raw observations to cancel out effects of satellite motion relative to the reference stations, effects of clocks, effects of troposphere and effects of ionosphere;
assigning the computed combination values into a plurality of nadir angle ranges, each nadir angle range being hereinafter referred to as an “angle bin”;
selecting a reference angle bin among the angle bins;
generating, for each angle bin, a representative combination value based on all the computed combination values that are associated with nadir angles that fall within said angle bin, wherein the representative combination value generated for the reference angle bin is a satellite-specific reference value that is constant over all nadir angles;
normalizing, for each angle bin, the representative combination value generated for the angle bin, based on a difference between the representative combination value generated for the reference angle bin and the representative combination value generated for the angle bin, to generate a normalized representative combination value for each angle bin;
generating the satellite-specific-nadir-angle-dependent-correction-information based on the normalized representative combination values; and
sending the satellite-specific-nadir-angle-dependent-correction-information to the NSS receiver for use in determining the position of the NSS receiver.

2. Method of claim 1 , wherein observing the NSS signals, on the basis of which the raw observations are obtained, comprises doing so over a plurality of consecutive days.

3. Method of claim 1 , wherein computing combination values comprises computing multipath combination values based on the raw observations to cancel out the effects of the satellite motion relative to the reference stations, the effects of the clocks, the effects of the troposphere and the effects of the ionosphere.

4. Method of claim 1 , wherein computing combination values comprises computing Melbourne-Wübbena combination values based on the raw observations to cancel out the effects of the satellite motion relative to the reference stations, the effects of the clocks, the effects of the troposphere and the effects of the ionosphere.

5. Method of claim 1 , wherein computing combination values comprises computing ionosphere-free pseudorange minus carrier phase (PC-LC) combination values based on the raw observations to cancel out the effects of the satellite motion relative to the reference stations, the effects of the clocks, the effects of the troposphere and the effects of the ionosphere.

6. Method of claim 1 , wherein computing combination values comprises computing geometry-free, also called “ionospheric”, pseudorange and carrier phase combinations based on the raw observations to cancel out the effects of the satellite motion relative to the reference stations, the effects of the clocks, and the effects of the troposphere; and using another information source to cancel out the effects of the ionosphere.

7. Method of claim 6 , wherein the other information source used to cancel out the effects of the ionosphere is an ionospheric map.

8. Method of claim 1 , wherein generating satellite-specific-nadir-angle-dependent-correction-information comprises generating at least one calibration table to be sent to a plurality of NSS receivers.

9. Method of claim 1 , wherein generating satellite-specific-nadir-angle-dependent-correction-information comprises generating coefficients for a polynomial expression, wherein the coefficients are to be sent to a plurality of NSS receivers.

10. 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 .

11. Method for generating correction information, hereinafter referred to as “satellite-specific-nadir-angle-dependent-correction-information”, associated with each of at least two navigation satellite system (NSS) satellites among a plurality of NSS satellites, wherein the satellite-specific-nadir-angle-dependent-correction-information associated with a NSS satellite comprises correction information depending on the nadir angle of a receiver as seen from the NSS satellite, so as to mitigate effects of satellite-specific, nadir-angle dependent biases in the NSS signals from the NSS satellite, the method comprising, for each NSS satellite among the at least two NSS satellites:
receiving raw observations obtained by observing NSS signals from the NSS satellite from a plurality of reference stations;
computing combination values based on the raw observations to cancel out effects of satellite motion relative to the reference stations, effects of clocks, effects of troposphere and effects of ionosphere;
assigning the computed combination values into a plurality of nadir angle ranges, each nadir angle range being hereinafter referred to as an “angle bin”;
selecting a reference angle bin among the angle bins;
generating, for each angle bin, a mean combination value by taking the average of all the computed combination values that are associated with nadir angles that fall within said angle bin, wherein the mean combination value generated for the reference angle bin is a satellite-specific reference value that is constant over all nadir angles;
normalizing, for each angle bin, the mean combination value generated for the angle bin, by subtracting the mean combination value generated for the reference angle bin from the mean combination value generated for the angle bin, to generate a normalized mean combination value for each angle bin;
generating the correction information based on the normalized mean combination values; and
sending the correction information to the NSS receiver for use in determining the position of the NSS receiver.

12. Apparatus configured for generating correction information for use by a global or regional navigation satellite system receiver, hereinafter abbreviated as NSS receiver, to determine a position of the NSS receiver, the correction information hereinafter referred to as “satellite-specific-nadir-angle-dependent-correction-information”, the satellite-specific-nadir-angle-dependent-correction-information associated with each of at least two navigation satellite system (NSS) satellites among a plurality of NSS satellites, wherein the satellite-specific-nadir-angle-dependent-correction-information associated with a NSS satellite comprises correction information depending on the nadir angle of a receiver as seen from the NSS satellite, so as to mitigate effects of satellite-specific, nadir-angle depe

Assignees

• Trimble Inc

Inventors

• Salazar Dagoberto
• Weinbach Ulrich
• Allison Timo

Classifications

• G01S19/072 Primary

  Ionosphere corrections · CPC title

• G01S19/073

  involving a network of fixed stations · CPC title

• G06F30/00

  Computer-aided design [CAD] · CPC title

• G01S19/42

  Determining position · CPC title

• G01S19/43

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