Granted Patent B2

US 12,395,237 · App. 17/813,099 · Granted Aug 19, 2025

Inventors: Kannan Muthuraman (Mission Viejo, CA); Francesco Grilli (La Jolla, CA)

Assignee: QUALCOMM Incorporated

H04B7/18547H04B7/18519H04B7/18541H04B7/18556

Abstract

Claims (104)

1. A method of facilitating pointing of a mobile device at a satellite of a satellite constellation for satellite-based data communication, the method comprising:

obtaining historical orbital data indicative of orbital movement of a set of satellites over a period of time, the set of satellites comprising at least a subset of satellites of the satellite constellation;

for each satellite in the set of satellites, estimating a set of orbital parameter values by fitting an orbital model to the historical data of the respective satellite, wherein at least one orbital parameter value of the set of orbital values is common across a group of satellites within the set of satellites; and

sending assistance data to at least one mobile device, the assistance data indicative of the respective set of orbital parameter values for all satellites of the set of satellites.

2. The method of claim 1 , wherein fitting the set of orbital parameter values for each satellite comprises:

estimating a preliminary set of orbital parameter values in a first operation of fitting the orbital model to a first portion of the historical data spanning a first portion of the period of time; and

using the preliminary set of orbital parameter values as seed values in a second operation of fitting the orbital model to a second portion of the historical data, wherein the second portion of the historical data spanning at least the first portion of the period of time.

3. The method of claim 2 , wherein at least one orbital parameter value common across the group of satellites is determined by the second operation of fitting the orbital model to the second portion of the historical data.

4. The method of claim 2 , wherein the historical data spanning the first portion of the period of time includes data spanning one or more steering events for each satellite in the set of satellites.

5. The method of claim 1 , wherein the group of satellites comprises:

satellites in a common orbital plane,

satellites in a common orbital shell, or

all satellites of the satellite constellation, or

a combination thereof.

6. The method of claim 1 , wherein the orbital model comprises a Keplerian model and the set of orbital parameter values comprises:

square-root of semi-major axis,

eccentricity,

mean anomaly,

inclination angle,

Right Ascension of Ascending Node (RAAN),

RAAN rate, or

argument of perigee, or

a combination thereof.

7. The method of claim 1 , wherein the orbital model comprises a equinoctial model and the set of orbital parameter values comprises:

semi-major axis,

components of an eccentricity vector in an equinoctial reference frame,

components of an ascending node vector in the equinoctial reference frame, or

mean longitude, or

a combination thereof.

8. The method of claim 1 , wherein obtaining the historical orbital data comprises uniformly sampling archived Two Line Element (TLE) data of the set of satellites for the period of time.

9. A device for facilitating pointing of a mobile device at a satellite of a satellite constellation for satellite-based data communication, the device comprising:

a transceiver;

a memory; and

one or more processors communicatively coupled with the transceiver and the memory, wherein the one or more processors are configured to:

obtain historical orbital data indicative of orbital movement of a set of satellites over a period of time, the set of satellites comprising at least a subset of satellites of the satellite constellation;

for each satellite in the set of satellites, estimate a set of orbital parameter values by fitting an orbital model to the historical data of the respective satellite, wherein at least one orbital parameter value of the set of orbital values is common across a group of satellites within the set of satellites; and

send assistance data to at least one mobile device, the assistance data indicative of the respective set of orbital parameter values for all satellites of the set of satellites.

10. The device of claim 9 , wherein the device comprises the mobile device or a computer server.

11. The device of claim 9 , wherein, to fit the set of orbital parameter values for each satellite, the one or more processors are configured to:

estimate a preliminary set of orbital parameter values in a first operation of fitting the orbital model to a first portion of the historical data spanning a first portion of the period of time; and

use the preliminary set of orbital parameter values as seed values in a second operation of fitting the orbital model to a second portion of the historical data, wherein the second portion of the historical data spanning at least the first portion of the period of time.

12. The device of claim 11 , wherein at least one orbital parameter value common across the group of satellites is determined by the second operation of fitting the orbital model to the second portion of the historical data.

13. The device of claim 11 , wherein, to obtain the historical data spanning the first portion of the period of time, the one or more processors are configured to obtain data spanning one or more steering events for each satellite in the set of satellites.

14. The device of claim 9 , wherein the group of satellites comprises:

satellites in a common orbital plane,

satellites in a common orbital shell, or

all satellites of the satellite constellation, or

a combination thereof.

15. The device of claim 9 , wherein the orbital model comprises a Keplerian model and the set of orbital parameter values comprises:

square-root of semi-major axis,

eccentricity,

mean anomaly,

inclination angle,

Right Ascension of Ascending Node (RAAN),

RAAN rate, or

argument of perigee, or

a combination thereof.

16. The device of claim 9 , wherein the orbital model comprises a equinoctial model and the set of orbital parameter values comprises:

semi-major axis,

components of an eccentricity vector in an equinoctial reference frame,

components of an ascending node vector in the equinoctial reference frame, or

mean longitude, or

a combination thereof.

17. The device of claim 9 , wherein, to obtain the historical orbital data, the one or more processors are configured to uniformly sample archived Two Line Element (TLE) data of the set of satellites for the period of time.

18. An apparatus for facilitating pointing of a mobile device at a satellite of a satellite constellation for satellite-based data communication, the apparatus comprising:

means for obtaining historical orbital data indicative of orbital movement of a set of satellites over a period of time, the set of satellites comprising at least a subset of satellites of the satellite constellation;

means for estimating, for each satellite in the set of satellites, a set of orbital parameter values by fitting an orbital model to the historical data of the respective satellite, wherein at least one orbital parameter value of the set of orbital values is common across a group of satellites within the set of satellites; and

means for sending assistance data to at least one mobile device, the assistance data indicative of the respective set of orbital parameter values for all satellites of the set of satellites.

19. The apparatus of claim 18 , wherein the means for fitting the set of orbital parameter values for each satellite comprises:

means for estimating a preliminary set of orbital parameter values in a first operation of fitting the orbital model to a first portion of the historical data spanning a first portion of the period of time; and

means for using the preliminary set of orbital parameter values as seed values in a second operation of fitting the orbital model to a second portion of the historical data, wherein the second portion of the historical data spanning at least the first portion of the period of time.

20. The apparatus of claim 19 , wherein at least one orbital parameter value common across the group of satellites is determined by the second operation of fitting the orbital model to the second portion of the historical data.

21. The apparatus of claim 19 , wherein the means for obtaining the historical data spanning the first portion of the period of time includes means for obtaining data spanning one or more steering events for each satellite in the set of satellites.

22. The apparatus of claim 18 , wherein the group of satellites comprises:

satellites in a common orbital plane,

satellites in a common orbital shell, or

all satellites of the satellite constellation, or

a combination thereof.

23. The apparatus of claim 18 , wherein the orbital model comprises a Keplerian model and the set of orbital parameter values comprises:

square-root of semi-major axis,

eccentricity,

mean anomaly,

inclination angle,

Right Ascension of Ascending Node (RAAN),

RAAN rate, or

argument of perigee, or

a combination thereof.

24. The apparatus of claim 18 , wherein the orbital model comprises a equinoctial model and the set of orbital parameter values comprises:

semi-major axis,

components of an eccentricity vector in an equinoctial reference frame,

components of an ascending node vector in the equinoctial reference frame, or

mean longitude, or

a combination thereof.

25. The apparatus of claim 18 , wherein the means for obtaining the historical orbital data comprises means for uniformly sampling archived Two Line Element (TLE) data of the set of satellites for the period of time.

26. A non-transitory computer-readable medium storing instructions for facilitating pointing of a mobile device at a satellite of a satellite constellation for satellite-based data communication, the instructions comprising code for:

obtaining historical orbital data indicative of orbital movement of a set of satellites over a period of time, the set of satellites comprising at least a subset of satellites of the satellite constellation;

for each satellite in the set of satellites, estimating a set of orbital parameter values by fitting an orbital model to the historical data of the respective satellite, wherein at least one orbital parameter value of the set of orbital values is common across a group of satellites within the set of satellites; and

sending assistance data to at least one mobile device, the assistance data indicative of the respective set of orbital parameter values for all satellites of the set of satellites.

27. The computer-readable medium of claim 26 , wherein the code for fitting the set of orbital parameter values for each satellite comprises code for:

estimating a preliminary set of orbital parameter values in a first operation of fitting the orbital model to a first portion of the historical data spanning a first portion of the period of time; and

using the preliminary set of orbital parameter values as seed values in a second operation of fitting the orbital model to a second portion of the historical data, wherein the second portion of the historical data spanning at least the first portion of the period of time.

28. The computer-readable medium of claim 27 , wherein at least one orbital parameter value common across the group of satellites is determined by the second operation of fitting the orbital model to the second portion of the historical data.

29. The computer-readable medium of claim 27 , wherein the code for obtaining the historical data spanning the first portion of the period of time includes code for obtaining data spanning one or more steering events for each satellite in the set of satellites.

30. The computer-readable medium of claim 26 , wherein the code for obtaining the historical orbital data comprises code for uniformly sampling archived Two Line Element (TLE) data of the set of satellites for the period of time.

Assignments (1)

Continuity (1)

References Cited (111)