System and method for providing accurate position location information to military forces in a disadvantaged signal environment
A system for determining a location in a disadvantaged signal environment includes three aerial vehicles hovering at high altitude and spaced apart to form a triangle, and a mother aerial vehicle positioned a distance away and at a lower altitude. The mother aerial vehicle acquires and transmits coarse geolocation information, using a pulse compression, high-power X Band radar and directional antenna, to each of the three aerial vehicles to direct them to coarse geo-positions above designated respective ground locations. One of the three aerial vehicles has a synthetic aperture radar for producing a terrain strip-map that is mensurated against a map database to provide fine position adjustments for each of the three aerial vehicles, which are also also configured to transmit a respective signal coded with its latitude, longitude, and altitude, for a computing device to perform time difference of arrival measurements of the signals to determine its location.
1. A method for determining if spoofing of global positioning system (GPS) signals is occurring in a region, said method comprising:
positioning first, second, and third aerial vehicles at a first altitude and at a stationary position in proximity to the region;
synchronizing the first, second, and third aerial vehicles with each other;
positioning a mother aerial vehicle a distance away from the first, second, and third aerial vehicles at a second altitude;
transmitting coarse geolocation information by the mother aerial vehicle to each of the first, second, and third aerial vehicles, thereby directing the first, second, and third aerial vehicles to respective coarse positions above a corresponding ground location in the region;
producing a terrain strip-map by one or more of the first, second, and third aerial vehicles and mensurating the terrain strip-map against a map database;
providing fine position adjustments to each of the first, second, and third aerial vehicles, based on said mensurated terrain strip map;
transmitting a respective coded signal by each of the first, second, and third aerial vehicles;
determining a location in the region by comparing time difference of arrival (TDOA) measurements of the respective coded signal at the location; and
determining if spoofing is occurring in the region by comparing said determined location with a GPS-derived location.
2. The method according to claim 1 , further comprising: coding each said respective coded signal with a latitude, a longitude, and an altitude of the respective aerial vehicle; and modulating each said respective coded signal with non-random, non-repeating patterns.
3. The method according to claim 2 , further comprising:
obtaining a mean sea level altitude; and
determining the location in the region using the mean sea level altitude and the TDOA measurements of the unique coded reference signals.
4. The method according to claim 3 , further comprising: synchronizing the first, second, and third aerial vehicles with the master aerial vehicle using frequency and timing data from a stable rubidium reference oscillator.
5. The method according to claim 4 , further comprising: synchronizing the first, second, and third aerial vehicles with the master aerial vehicle by operating the stable rubidium reference oscillator in the range of 425 MHz to 2.4 GHz.
6. The method according to claim 5 , further comprising: transmitting each said coded signal over an ISM band frequency.
7. The method according to claim 6 , further comprising: refreshing each said respective coded signal at a rate of 5 Hz.
8. The method according to claim 7 , further comprising: mensurating the strip-map against one or more of:
a level two digital terrain elevation map dataset; and
a google earth map by said master aerial vehicle.
9. The method according to claim 8 , further comprising: transmitting the coarse geolocation information from the mother aerial vehicle to each of the first, second, and third aerial vehicles via an X-Band link.
10. The method according to claim 9 , further comprising: transmitting the coarse geolocation information from the mother aerial vehicle to each of the first, second, and third aerial vehicles using a pulse compression, high-power X Band radar with a directional antenna, using a beam width of about one degree with sidelobe levels of less than 40 dB.
11. The method according to claim 10 , further comprising: increasing jam resistance by transmitting the coarse geolocation information with the directional antenna using frequency hopping spread spectrum waveforms.
12. The method according to claim 11 , further comprising: positioning the first, second, and third aerial vehicles at a higher altitude than the mother aerial vehicle.
13. The method according to claim 12 , further comprising: spacing the first, second, and third aerial vehicles between five miles and ten miles apart.
14. The method according to claim 13 , further comprising: positioning the first, second, and third aerial vehicles at an altitude being above a range capability of anti-aircraft artillery gunfire.
15. The method according to claim 14 , further comprising: positioning the mother vehicle at an altitude being less than 10,000 feet AGL.
16. A method of providing jam-resistant and spoof-resistant position information to a mission participant in a disadvantaged signal environment at a covert location, said method comprising:
positioning each of a first aerial vehicle, a second aerial vehicle, and a master aerial vehicle at a preset altitude and at a stationary position in proximity to the covert location;
positioning a mother aerial vehicle at a predetermined altitude and at a distance away from the disadvantaged signal environment of the covert location;
synchronizing the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle using frequency and timing information;
measuring an initial position of the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle, by the mother aerial vehicle, using an onboard high resolution radar;
transmitting two locations from the mother aerial vehicle to the master aerial vehicle, via an X band link with a very narrow beam width and extremely low side lobe levels, including: transmitting said measured initial position, and transmitting respective spaced-apart positions above the covert location for each of the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle;
maneuvering the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle to the respective spaced-apart positions;
acquiring respective fine position adjustments for each of the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle, by producing a terrain strip-map using a synthetic aperture radar on the master air vehicle, and mensurating the terrain strip-map against a map database;
transmitting the respective fine position adjustments from the master aerial vehicle to the first aerial vehicle and the second aerial vehicle;
maneuvering the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle to its respective fine-adjusted position;
coding, by each of the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle, a unique reference signal including its latitude, longitude, and altitude transmitting, by each of the first aerial vehicle, the second aerial vehicle, and the master aerial vehicle, its unique coded reference signal;
determining a geo-location of the mission participant by performing time difference of arrival (TDOA) measurements of the unique coded reference signals, using a computing device.
17. The method according to claim 16 , further comprising:
obtaining a mean sea level altitude of the mission participant by determining a pressure altitude using a barometric sensor, and converting said determined pressure altitude to the mean sea level altitude a using the computing device;
determining the geo-location of the mission participant using the time difference of arrival (TDOA) measurements of the unique coded reference signals in combination with the obtained mean sea level altitude.
18. The method according to claim 17 , further comprising:
coding the unique reference signal using direct sequence coding.
19. The method according to claim 17 , further comprising:
coding the unique reference signal using frequency hopping (FH/SS) coding.
20. The method according to claim 16 , further comprising:
determining if spoofing of global positioning system (GPS) signals is occurring at the covert location by comparing said determined geo-location from the TDOA measurements with a GPS-derived location.