Method for selecting a satellite

Patent metadata

Field	Value
Publication number	US-9903956-B2
Application number	US-201214344440-A
Country	US
Kind code	B2
Filing date	Sep 12, 2012
Priority date	Sep 12, 2011
Publication date	Feb 27, 2018
Grant date	Feb 27, 2018

Abstract

The invention relates to a method for selecting a satellite which is designed to send a global navigation satellite system-signal, also known as a GNSS-Signal, to a vehicle, consisting of: measuring measurement position data of the vehicle in relation to the satellite based on the GNSS-Signal; determining redundant reference position data of the vehicle in relation to the measurement position data determined according to the GNSS-Signal; and selecting the satellite when a comparison of the measurement position data and the reference position data meets a predetermined condition.

First claim

The invention claimed is:

1. A method for selecting a satellite that is designed to send a global navigation satellite system (“GNSS”) signal to a vehicle, the method comprising:
measuring measurement location data for the vehicle with respect to the satellite on the basis of the GNSS signal,
determining reference location data for the vehicle that are redundant relative to the measurement location data determined on the basis of the GNSS signal; and
selecting the satellite as a source for the GNSS signal for the vehicle when a juxtaposition of the measurement location data and the reference location data satisfies a predetermined condition;
wherein the predetermined condition is a maximum admissible error between the measurement location data and the reference location data; and
wherein the maximum admissible error is dependent on a standard deviation that is calculated on the basis of a sum comprising a reference variance for the reference location data and a measurement variance for the measurement location data, wherein the maximum admissible error between the measurement location data and the reference location data and noise in the measurement location data and the reference location data correlate.

2. The method as claimed in claim 1 , wherein the juxtaposition of the measurement location data and the reference location data involves a difference being formed between the measurement location data and the reference location data.

3. The method as claimed in claim 1 , wherein the maximum admissible error corresponds to a multiple of the standard deviation, wherein a probability that the measurement location data are below a predetermined threshold value in a scatter range is dependent on the standard deviation.

4. The method as claimed in claim 1 , wherein the measurement location data for the vehicle and the reference location data for the vehicle each comprise a distance from the satellite or a relative speed in the visual direction of the satellite.

5. The method as claimed in claim 4 , wherein the distance from the satellite or the relative speed in the visual direction of the satellite is determined from a code measurement and a phase measurement for the GNSS signal.

6. The method as claimed in claim 1 , wherein the reference location data are dependent on driving dynamics data or odometry data for the vehicle.

7. A method for selecting a satellite that is designed to send a global navigation satellite system (“GNSS”) signal to a vehicle, the method comprising:
recording of locations for at least three satellites relative to each other from a point of view of the vehicle, said satellites comprising the satellite to be selected, wherein the locations include distances between each of the at least three satellites with respect to one another;
measuring measurement location data for the vehicle with respect to at least two of the at least three satellites on the basis of GNSS signals received at the vehicle from the at least two of the at least three satellites, wherein the measurement location data includes distances between the vehicle and the at least two of the at least three satellites,
selecting at least one of the at least two satellites as a source for the GNSS signal for the vehicle when the locations of the three satellites relative to one another from the point of view of the vehicle and the measurement location data correlate, and
eliminating or ignoring at least one of the at least two satellites as the source for the GNSS signal for the vehicle when the locations of the three satellites relative to one another from the point of view of the vehicle and a location of the at least one of the at least two satellites derived from the measurement location data do not correlate.

8. A control apparatus, the control apparatus comprising:
a processor;
a memory in communication with the processor, the memory having instructions stored thereon that, when executed by the processor, configure the processor to:
measure measurement location data for a vehicle with respect to the satellite on the basis of global navigation satellite system (“GNSS”) signal, and
select the satellite as a source for the GNSS signal for the vehicle when the measurement location data satisfy a predetermined condition;
wherein the predetermined condition is a maximum admissible error between the measurement location data and a reference location data; and
wherein the maximum admissible error is dependent on a standard deviation that is calculated on the basis of a sum comprising a reference variance for the reference location data and a measurement variance for the measurement location data, wherein the maximum admissible error between the measurement location data and the reference location data and noise in the measurement location data and the reference location data correlate.

9. The control apparatus of claim 8 , wherein the processor is further configured to:
determine reference location data for the vehicle that are redundant relative to the measurement location data determined on the basis of the GNSS signal; and
select the satellite when the measurement location data and the reference location data satisfies the predetermined condition.

Assignees

• Steinhardt Nico
• Continental Teves Ag & Co Ohg

Inventors

• Steinhardt Nico

Classifications

• G01S19/22 Primary

  Multipath-related issues · CPC title

• G01S19/28 Primary

  Satellite selection · CPC title

• G01S19/215

  issues related to spoofing · CPC title

• G01S19/21

  Interference related issues {; Issues related to cross-correlation, spoofing or other methods of denial of service} · CPC title

• G01S19/20 Primary

  Integrity monitoring, fault detection or fault isolation of space segment · CPC title