Receiver design for doppler positioning with low earth orbit satellites and differential carrier phase measurements

Patent metadata

Field	Value
Publication number	US-11960018-B2
Application number	US-202017604154-A
Country	US
Kind code	B2
Filing date	Apr 15, 2020
Priority date	Apr 15, 2019
Publication date	Apr 16, 2024
Grant date	Apr 16, 2024

Abstract

System and device configurations, and processes are provided for determining position based on low Earth orbit (LEO) satellite signals. Frameworks described herein can include performing Doppler frequency measurement for received quadrature phase shift keying (QPSK) signals. The framework may include channel tracking operations to determine Doppler shift measurements, a navigation filter operation to determine clock drift based on each Doppler shift measurement from each channel tracking loop, and determining position of a device based on LEO satellite signal sources. Frameworks described herein are also provided for 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. Embodiments can also cancel effects of ionospheric and tropospheric delays on the carrier phase and CD-LEO measurements.

First claim

What is claimed is:

1. A method for determining position based on low Earth orbit (LEO) satellite signals, the method comprising:
receiving, by a device, one or more low earth orbit (LEO) satellite signals, wherein the LEO satellite signals include direct quadrature phase shift keying (QPSK) signals;
performing, by the device, a Doppler frequency measurement for the quadrature phase shift keying (QPSK) signals for each downlink channel received, wherein the Doppler frequency measurement includes
filtering each received downlink channel, and
performing a channel tracking operation for each filtered downlink channel, the channel tracking operation including an independent phase-lock loop to track each filtered downlink signal, wherein each phase-lock loop determines a Doppler shift measurement; and

performing, by the device, a navigation filter operation to determine clock drift based on each Doppler shift measurement from each channel tracking loop; and
determining, by the device, a position of the device, wherein the device determines position based on clock drift determined by the navigation filter operation and tracking data for each LEO satellite signal source.

2. The method of claim 1 , wherein the channel tracking operation provides a downlink channel Doppler frequency estimate to the navigation filter operation to determine clock drift between a LEO satellite and the device.

3. The method of claim 1 , wherein the channel tracking operation includes an integrate and dump filter, a channel phase discriminator, and a channel loop filter in series, and a feedback loop including a numerically controller oscillator.

4. The method of claim 1 , wherein determining a position of the device is based on altimeter data detected for the device, and LEO satellite data including a velocity vector and position for each LEO satellite.

5. The method of claim 1 , wherein the navigation filter operation includes at least one of an extended Kalman filter and weighted non-linear least-squares (WNLS) estimator.

6. The method of claim 1 , further comprising receiving base receiver position data and carrier phase data from a base receiver, wherein position of the device is determined based on a carrier phase differential operation with the base receiver position data and the carrier phase data as input.

7. The method of claim 6 , wherein the base receiver is at least one of a mobile receiver and stationary receiver, and wherein the device is configured to receive the base receiver position data and carrier phase data from the base receiver.

8. The method of claim 1 , wherein determining position includes canceling at least one of ionospheric delay and toropospheric delay from received satellite signals.

9. The method of claim 1 , wherein position is determined for the device when stationary and measurement collected at different times in a batch estimator.

10. The method of claim 1 , wherein a double-difference operation is performed to obtain carrier phase measurement differences from multiple LEO satellites.

11. A device configured to determine position based on low Earth orbit (LEO) satellite signals, the device comprising:
a communications module configured to receive one or more low earth orbit (LEO) satellite signals, wherein the LEO satellite signals include direct quadrature phase shift keying (QPSK) signals; and
a controller, coupled to the communications module, wherein the controller is configured to
perform a Doppler frequency measurement for the quadrature phase shift keying (QPSK) signals for each downlink channel received, wherein the Doppler frequency measurement includes
filter each received downlink channel, and
performing a channel tracking operation for each filtered downlink channel, the channel tracking operation including an independent phase-lock loop to track each filtered downlink signal, wherein each phase-lock loop determines a Doppler shift measurement; and

perform a navigation filter operation to determine clock drift based on each Doppler shift measurement from each channel tracking loop; and
determine a position of the device, wherein the device determines position based on clock drift determined by the navigation filter operation and tracking data for each LEO satellite signal source.

12. The device of claim 11 , wherein the channel tracking operation provides a downlink channel Doppler frequency estimate to the navigation filter operation to determine clock drift of the device.

13. The device of claim 11 , wherein the channel tracking operation includes an integrate and dump filter, a channel phase discriminator, and a channel loop filter in series, and a feedback loop including a numerically controller oscillator.

14. The device of claim 11 , wherein determining a position of the device is based on altimeter data detected for the device, and LEO satellite data including a velocity vector and position for each LEO satellite.

15. The device of claim 11 , wherein the navigation filter operation includes at least one of an extended Kalman filter and weighted non-linear least-squares (WNLS) estimator.

16. The device of claim 11 , further comprising receiving base receiver position data and carrier phase data from a base receiver, wherein position of the device is determined based on a carrier phase differential operation with the base receiver position data and the carrier phase data as input.

17. The device of claim 16 , wherein the base receiver is at least one of a mobile receiver and stationary receiver, and wherein the device is configured to receive the base receiver position data and carrier phase data from the base receiver.

18. The device of claim 11 , wherein determining position includes canceling at least one of ionospheric delay and toropospheric delay from received satellite signals.

19. The device of claim 11 , wherein position is determined for the device when stationary and measurement collected at different times in a batch estimator.

20. The device of claim 11 , wherein a double-difference operation is performed to obtain carrier phase measurement differences from multiple LEO satellites.

Assignees

• Univ California

Inventors

• Kassas Zak
• Khalife Joe
• Abdallah Ali

Classifications

• G01S19/38

  Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system · CPC title

• G01S5/0284 Primary

  Relative positioning · CPC title

• G01S5/0246

  involving frequency difference of arrival or Doppler measurements (G01S5/02685 takes precedence) · CPC title

• G01S5/009 Primary

  Transmission of differential positioning data to mobile · CPC title