Determination of a ground receiver position

Patent metadata

Field	Value
Publication number	US-10024946-B2
Application number	US-201715610597-A
Country	US
Kind code	B2
Filing date	May 31, 2017
Priority date	Sep 26, 2014
Publication date	Jul 17, 2018
Grant date	Jul 17, 2018

Abstract

Technology for determining a geographical location of a ground receiver is disclosed. A plurality of radio frequency (RF) signals from a plurality of RF signal carriers may be received at the ground receiver. The plurality of RF signal carriers may include satellites operated by a foreign entity or non-global positioning system (non-GPS) satellites. The ground receiver may measure a Doppler shift associated with each of the plurality of RF signals. The geographical location of the ground receiver may be determined in X, Y and Z coordinates based in part on the Doppler shift associated with each of the plurality of RF signals.

First claim

What is claimed is:

1. A method for determining a geographical location of a ground receiver, the method comprising:
receiving a first radio frequency (RF) signal, at the ground receiver from an RF signal carrier;
receiving a second RF signal, at the ground receiver from a relay satellite, wherein the second RF signal is a transponded RF signal, wherein the relay satellite receives a GPS signal from a GPS satellite and shifts a frequency of the GPS signal to create the second RF signal or the relay satellite receives a RF signal from the RF signal carrier and shifts a frequency of the second RF signal to create the second RF signal;
calculating a first range (R1) that represents a distance traveled by the first RF signal between the RF signal carrier and the ground receiver;
calculating a third range (R3) that represents a distance traveled by the second RF signal between the relay satellite and the ground receiver, wherein a second range (R2) represents a distance between the RF signal carrier and the relay satellite and a GPS range (G1) represents a distance traveled by the GPS signal between the GPS satellite and the relay satellite; and
determining the geographical location of the ground receiver based in part on the first range (R1), the second range (R2), the third range (R3) and the GPS range (G1).

2. The method of claim 1 , further comprising:
calculating a first Doppler shift associated with the first RF signal received at the ground receiver from the RF signal carrier;
calculating a second Doppler shift associated with the second RF signal received at the ground receiver from the relay satellite, wherein the second RF signal has an increased Doppler shift with respect to the RF signal and the GPS signal; and
determining the geographical location of the ground receiver based in part on the first Doppler shift, the second Doppler shift, the first range (R1), the second range (R2), the third range (R3) and the GPS range (G1).

3. The method of claim 1 , further comprising:
measuring a time of flight (T) for the GPS signal to arrive at the ground receiver from the GPS satellite by decoding the second RF signal to determine a GPS ephemeris and GPS time; and
calculating an estimate of R3 using T=(G1+R3)/c+d,
wherein c is the speed of light,
wherein G1 is predetermined, and
wherein d is a measured time delay representing an amount of time for the relay satellite to receive the GPS signal from the GPS satellite or receive the RF signal from the RF signal carrier, shift a frequency associated with the GPS signal or the RF signal to create the second RF signal, and send the second RF signal to the ground receiver.

4. The method of claim 3 , further comprising calculating R1 using (R2+R3)/c+d=(R1/c)+t, wherein t represents a time lag between the ground receiver receiving the second RF signal from the relay satellite with respect to receiving the first RF signal from the RF signal carrier, wherein R2 is predetermined.

5. The method of claim 1 , further comprising:
receiving a plurality of global position system (GPS) signals from one or more GPS satellites;
determining the geographical location of the ground receiver based in part on the plurality of GPS signals; and
determining an orbit for each of a plurality of RF signal carriers using the geographical location of the ground receiver.

6. The method of claim 1 , wherein the geographical position and ephemeris for each of the GPS satellite, RF signal carrier and relay satellite is known to the ground receiver.

7. The method of claim 1 , wherein the RF signal carrier includes at least one of low Earth orbit (LEO) satellites, medium Earth orbit (MEO) satellites or geostationary (GEO) satellites.

8. The method of claim 1 , wherein the RF signal carrier comprises a GPS satellite.

9. The method of claim 1 , wherein the RF signal carrier comprises a non-dedicated satellite.

10. The method of claim 1 , wherein the RF signals are not global positioning system (GPS) signals or ranging signals.

11. The method of claim 1 , wherein the relay satellite is selected from a group consisting of a cube satellite (CUBESAT), a picosatellite, a nanosatellite, and a microsatellite, wherein the CUBESAT weighs less than 5 kilograms.

12. A ground receiver operable to determine a geographical location of the ground receiver; the ground receiver having computer circuitry configured to:
receive a first radio frequency (RF) signal, at the ground receiver from an RF signal carrier;
receive a third RF signal, at the ground receiver from a relay satellite, wherein the third RF signal is a transponded RF signal, wherein the relay satellite receives a second RF signal from the RF signal carrier and shifts a frequency of the second RF signal to create the third RF signal;
calculate a first range (R1) that represents a distance traveled by the first RF signal between the RF signal carrier and the ground receiver,
calculate a third range (R3) that represents a distance traveled by the third RF signal between the relay satellite and the ground receiver, wherein a second range (R2) represents a distance between the RF signal carrier and the relay satellite; and
determine the geographical location of the ground receiver based in part on the first range (R1), the second range (R2), and the third range (R3).

13. The ground receiver of claim 12 , further configured to determine the geographical location of the ground receiver using (R2+R3)/c+d=(R1/c)+t,
wherein c is a speed of light,
wherein R2 is predetermined,
wherein d is a measured time delay representing an amount of time for the relay satellite to receive the second RF signal from the RF signal carrier, shift a frequency associated with the second RF signal to create the third RF signal, and send the third RF signal to the ground receiver, and
t represents a time lag between the ground receiver receiving the third RF signal from the relay satellite with respect to receiving the first RF signal from the RF signal carrier.

14. The ground receiver of claim 12 , wherein R1 minus R3 is a constant and R3 is conditional on R1.

15. The ground receiver of claim 12 , wherein the first RF signal and the second RF signal are not global positioning system (GPS) signals.

16. The ground receiver of claim 12 , wherein the RF signal carrier includes at least one non-dedicated satellite that is operated by a foreign entity or is a non-global positioning system (non-GPS) satellite.

Assignees

• Raytheon Co

Inventors

• Robinson Ian S
• Hautzik Andrew M
• Crow Brandon

Classifications

• G01S19/11

  wherein the cooperating elements are pseudolites or satellite radio beacon positioning system signal repeaters · CPC title

• G01S19/215

  issues related to spoofing · CPC title

• G01S1/02 Primary

  using radio waves (G01S19/00 takes precedence) · CPC title

• G01S19/21

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

• G01S19/10

  providing dedicated supplementary positioning signals · CPC title