Navigation satellite system positioning with enhanced satellite-specific correction information
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.
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.