IP Library › Granted Patent US 10,768,264
Granted Patent B2
US 10,768,264 · App. 16/036,818 · Granted Sep 8, 2020

Determination of a ground receiver position

Inventors: Ian S. Robinson (Redondo Beach, CA); Andrew M. Hautzik (Rancho Palos Verdes, CA); Brandon Crow (Gardena, CA)
Assignee: Raytheon Company
G01S1/02G01S19/10G01S19/11G01S19/21G01S19/215G01S19/48
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Quick Facts
Patent No.
US 10,768,264
App. No.
16/036,818
Granted
Sep 8, 2020
Kind
B2
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.

Claims (11)

1. A ground receiver operable to determine a geographical location of the ground receiver, the ground receiver having computer circuitry configured to:

receive a plurality of radio frequency (RF) signals from a plurality of RF signal carriers at the ground receiver, wherein the plurality of RF signal carriers include at least one non-dedicated satellite, wherein the at least one non-dedicated satellite is a non-global positioning system (non-GPS) satellite;

measure a Doppler shift associated with each of the plurality of RF signals at the ground receiver, wherein the computer circuitry is further configured to:

measure frequencies for each of a plurality of non-spread spectrum RF signals;

compare the frequencies to known frequencies associated with the plurality of non-spread spectrum RF signals;

calculate a difference between the frequencies that are measured and the known frequencies in order to calculate the Doppler shift for each of the non-spread spectrum RF signals; and

determine the geographical location of the ground receiver in X, Y and Z coordinates based in part on the Doppler shift associated with each of the plurality of RF signals.

2. The ground receiver of claim 1 , wherein the RF signal carriers comprise at least one of low Earth orbit (LEO) satellites, medium Earth orbit (MEO) satellites or geostationary (GEO) satellites.

3. The ground receiver of claim 1 , wherein the RF signals comprise RF signals other than global positioning system (GPS) signals or ranging signals.

4. The ground receiver of claim 1 , wherein the computer circuitry of the ground receiver is further configure to determine an oscillator offset associated with the ground receiver, wherein the oscillator offset includes a frequency drift in a local oscillator of the ground receiver.

5. The ground receiver of claim 1 , wherein the computer circuitry of the ground receiver is further configure to determine, at the ground receiver, source locations associated with the plurality of RF signal carriers and the frequencies associated with the plurality of RF signals prior to determining the geographical location of the ground receiver.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 17, 2019
From: ROBINSON, IAN S; CROW, BRANDON
To: RAYTHEON COMPANY
Reel/Frame 049485/0197 →
Continuity (3)
Division 15610597 · May 31, 2017
Division 14498069 · Sep 26, 2014
Related Publication 20180329013A1 · Nov 15, 2018