Differential emitter geolocation
An unknown location of a transmitter of interest is determined based on wireless signals transmitted by both the transmitter of interest and a reference transmitter positioned at a known location. The transmitted signals are received at a plurality of non-earthbound platforms each moving in a known manner, and phase measurements for each received signal are used to determine the unknown location.
1. A method of geolocating a wireless transmitter located on earth, comprising:
receiving, at a plurality of non-earthbound platforms each moving in a known manner within a spatial coordinate system, a frequency carrier transmitted from a first wireless transmitter whose location within the spatial coordinate system is unknown;
receiving, at said plurality of platforms, a frequency carrier transmitted from a reference wireless transmitter whose location within the spatial coordinate system is known;
for each of the received frequency carriers, at each of the platforms, obtaining first and second instantaneous phase measurements at first and second times, respectively;
for each of the platforms, determining a first difference between the first phase measurement associated with the first transmitter and the first phase measurement associated with the reference transmitter;
for each of the platforms, determining a second difference between the second phase measurement associated with the first transmitter and the second phase measurement associated with the reference transmitter; and
using said first and second differences to determine the location of the first transmitter.
2. The method of claim 1 , wherein said using includes determining, with respect to one of the platforms, a plurality of third differences, determining, with respect to one of the platforms, a plurality of fourth differences, and using the plurality of third differences and the plurality of fourth differences to determine the location of the first transmitter, wherein each said third difference is a difference between the first difference determined for the associated platform and the first difference determined for a respective one of the other platforms, and wherein each said fourth difference is a difference between the second difference determined for the associated platform and the second difference determined for a respective one of the other platforms.
3. The method of claim 1 , wherein each said platform is a satellite platform moving in space beyond earth atmosphere.
4. The method of claim 1 , wherein each said platform is an airborne platform moving in earth atmosphere.
5. The method of claim 1 , wherein said obtaining includes, for each of the platforms, using an associated phase locked loop to obtain the first and second instantaneous phase measurements at the first and second times, respectively.
6. The method of claim 1 , wherein the plurality of platforms includes at least four platforms.
7. The method of claim 1 , wherein said obtaining includes obtaining a third instantaneous phase measurement at a third time.
8. The method of claim 1 , wherein the frequency carriers are radio frequency (RF) carriers.
9. A system for geolocating a transmitter located on earth, comprising:
a plurality of non-earthbound platforms each moving in a known manner within a spatial coordinate system, each said platform containing a measurement unit configured to obtain first and second instantaneous phase measurements at first and second times, respectively, for a received frequency carrier transmitted from a first wireless transmitter whose location within the spatial coordinate system is unknown, each said measurement unit further configured to obtain first and second instantaneous phase measurements at said first and second times, respectively, for a received frequency carrier transmitted from a reference wireless transmitter whose location within the spatial coordinate system is known; and
a combiner coupled to said platforms and configured to determine, for each of the platforms, a first difference between the first phase measurement associated with the first transmitter and the first phase measurement associated with the reference transmitter, said combiner further configured to determine, for each of the platforms, a second difference between the second phase measurement associated with the first transmitter and the second phase measurement associated with the reference transmitter, and said combiner configured to use said first and second differences to determine the location of the first transmitter.
10. The system of claim 9 , wherein said combiner is configured to determine, with respect to one of the platforms, a plurality of third differences, to determine, with respect to one of the platforms, a plurality of fourth differences, and to use the plurality of third differences and the plurality of fourth differences to determine the location of the first transmitter, wherein each said third difference is a difference between the first difference determined for the associated platform and the first difference determined for a respective one of the other platforms, and wherein each said fourth difference is a difference between the second difference determined for the associated platform and the second difference determined for a respective one of the other platforms.
11. The system of claim 9 , wherein each said platform is a satellite platform moving in space beyond earth atmosphere.
12. The system of claim 9 , wherein each said platform is an airborne platform moving in earth atmosphere.
13. The system of claim 9 , wherein each said measurement unit has an associated phase locked loop for obtaining the first and second instantaneous phase measurements at the first and second times, respectively.
14. The system of claim 9 , wherein the plurality of platforms includes at least four platforms.
15. The system of claim 9 , wherein each said measurement unit is configured to obtain, for each of said carriers, a third instantaneous phase measurement at a third time.
16. The system of claim 9 , wherein the frequency carriers are RF carriers.