Navigation with differential carrier phase measurement from low earth orbit satellites
View Patent ↗Systems, device configurations, and processes are provided for navigation and determination of navigation observables based on low Earth orbit (LEO) satellite signals. A method for navigation includes using differential carrier phase measurement of LEO signals including correction of position estimates using integer ambiguity resolution and double difference carrier phase determinations. Frameworks described herein can use a computationally efficient integer ambiguity resolution to reduce the size of the integer least squares (ILS) determination. The framework may include a joint probability density function (pdf) of the megaconstellation LEO satellites' azimuth and elevation angle to characterize a LEO system. Embodiments are also directed to correction of ambiguities of carrier phase differential (CD)-low Earth orbit (LEO) (CD-LEO) measurements that may utilize a base and a rover without requiring prior knowledge of rover position.
1. A method for navigation using differential carrier phase measurement of low earth orbit (LEO) satellite signals, the method comprising:
receiving, by a device, one or more low earth orbit (LEO) satellite signals;
receiving, by the device, observables for the one or more LEO satellite signals from a base;
determining, by the device, a position estimate for the device using carrier phase determinations of the one or more LEO satellite signals received by the device and the observables from the base;
correcting, by the device, the position estimate, wherein correcting is based on an integer ambiguity resolution operation and double difference carrier phase determination for the one or more LEO satellite signals; and
determining, by the device, at least one navigation observable using a corrected position estimate.
2. The method of claim 1 , wherein the device receives signals from at least two LEO satellite vehicles, and wherein receiving includes receiving estimates of LEO satellite vehicle position.
3. The method of claim 1 , wherein the device receives base position and carrier phase observables determined by the base, the base having a known position.
4. The method of claim 1 , wherein determining a position estimate includes determining a position estimate for the device in at least one of a stationary and moving state.
5. The method of claim 1 , wherein determining a position estimate includes performing a batch-weighted nonlinear least squares (B-WNLS) operation over a window of steps.
6. The method of claim 1 , wherein determining a position estimate includes performing an extended Kalman filter operation to estimate position and velocity of the device from single difference measurements.
7. The method of claim 1 , wherein carrier phase determinations include differential carrier phase measurements using a simultaneous tracking and navigation framework (STAN) to estimate LEO satellite vehicle states.
8. The method of claim 1 , wherein correcting the position estimate includes performing a point-solution weighted non-linear least squares (PS-WNLS) estimator to estimate rover position in real time.
9. The method of claim 1 , wherein correcting the position estimate includes performing a joint probability density function (pdf) of megaconstellation LEO satellite azimuth and elevation angles to characterize a LEO satellite sources.
10. The method of claim 1 , wherein the navigation observable includes real-time position of the device.
11. A device configured for navigation using differential carrier phase measurement of low earth orbit (LEO) satellites, the device comprising:
a receiver configured to
receive one or more low earth orbit (LEO) satellite signals, and
receive observables for the one or more LEO satellite signals from a base; and
a controller configured to
determine a position estimate for the device using carrier phase determinations of the one or more LEO satellite signals received by the device and the observables from the base;
correct the position estimate, wherein correcting is based on an integer ambiguity resolution operation and double difference carrier phase determination for the one or more LEO satellite signals; and
determine at least one navigation observable using a corrected position estimate.
12. The device of claim 11 , wherein the receiver receives signals from at least two LEO satellite vehicles, and wherein receiving includes receiving estimates of LEO satellite vehicle position.
13. The device of claim 11 , wherein the receiver receives base position and carrier phase observables determined by the base, the base having a known position.
14. The device of claim 11 , wherein determining a position estimate includes determining a position estimate for the device in at least one of a stationary and moving state.
15. The device of claim 11 , wherein determining a position estimate includes performing a batch-weighted nonlinear least squares (B-WNLS) operation over a window of steps.
16. The device of claim 11 , wherein determining a position estimate includes performing an extended Kalman filter operation to estimate position and velocity of the device from single difference measurements.
17. The device of claim 11 , wherein carrier phase determinations include differential carrier phase measurements using a simultaneous tracking and navigation framework (STAN) to estimate LEO satellite vehicle states.
18. The device of claim 11 , wherein correcting the position estimate includes performing a point-solution weighted non-linear least squares (PS-WNLS) estimator to estimate rover position in real time.
19. The device of claim 11 , wherein correcting the position estimate includes performing a joint probability density function (pdf) of megaconstellation LEO satellite azimuth and elevation angles to characterize a LEO satellite sources.
20. The device of claim 11 , wherein the navigation observable includes real-time position of the device.