Satellite antenna station keeping

• US 6,989,786 B1
• Filed: 06/30/2004
• Issued: 01/24/2006
• Est. Priority Date: 06/30/2004
• Status: Active Grant

• Current Assignee: Intelsat Global Service Corporation
• Original Assignee: Intelsat Global Service Corporation
• Inventors: Dong, Guibin
• Primary Examiner(s): PHAN, DAO LINDA
• Application Number:
  US10/879,706
• Time in Patent Office: 573 Days
• Field of Search: 342/81, 342/154, 342/157, 342/352, 342/354
• US Class Current: 342/354
• CPC Class Codes: H04B 7/18515 Transmission equipment in satellites or space-based relays

Abstract

Techniques for redirecting a satellite antenna beam from a satellite antenna of a satellite in an inclined orbit to a preferred satellite antenna beam pointing position on the earth are provided. Satellite antenna maneuver data is computed based upon information associated with the satellite, such as telemetry, orbital, and antenna nominal pointing information. Command code sequences are then generated that correspond to the maneuver data. The command codes are executable at the inclined orbit satellite to modify the antenna position. The generated command codes are then transmitted to the inclined orbit satellite to redirect the satellite antenna beam center to the preferred position.

Claims

1. A method for redirecting a satellite antenna beam from a satellite antenna of an inclined orbit satellite to a nominal satellite antenna beam pointing position on the earth'"'"'s surface, comprising:

computing satellite antenna maneuver data based upon telemetry, orbital, and antenna nominal pointing information associated with the inclined orbit satellite;

generating command code sequences corresponding to the generated maneuver data executable at the inclined orbit satellite to modify azimuth and elevation angles of the satellite antenna; and

transmitting, to the inclined orbit satellite, the generated command code sequences to redirect the satellite antenna beam center close to the nominal satellite antenna beam pointing position on the earth'"'"'s surface.

2. The method of claim 1, wherein:

the satellite telemetry, orbital, and antenna nominal pointing information includes satellite attitude data, satellite orbit element data, and one of i) the nominal satellite antenna beam pointing position on the earth'"'"'s surface and ii) a nominal satellite antenna beam pointing position on the satellite;

the nominal satellite antenna beam pointing position on the earth'"'"'s surface corresponds to a target latitude and target longitude; and

the nominal satellite antenna beam pointing position on the satellite corresponds to target azimuth and target elevation angles of the satellite antenna.

3. The method of claim 2, wherein the satellite orbit element data includes a plurality of satellite orbit parameters.

4. The method of claim 1, wherein the computed satellite antenna maneuver data includes data indicating a number of satellite antenna maneuvers to be performed in a time period, a time at which to perform each of the number of satellite antenna maneuvers, and azimuth and elevation angles for each of the number of satellite antenna maneuvers.

5. The method of claim 1, wherein the satellite antenna maneuver data is computed by performing a plurality of coordinate frame transformations.

6. The method of claim 5, wherein performing the plurality of coordinate frame transformations includes:

performing an earth station top centric frame to satellite centric frame transformation based on the nominal satellite antenna beam pointing position on the earth'"'"'s surface and a satellite inclination value of zero to define first parameters;

performing a satellite centric frame to earth centric frame transformation based on the defined first parameters and the actual satellite inclination value to define second parameters;

performing an earth station top centric frame to satellite centric frame transformation based upon the defined first and second parameters and the actual satellite inclination value to generate a first portion of the antenna maneuver data; and

performing a satellite centric frame to earth centric frame transformation based upon the first portion of the antenna maneuver data to generate a second portion of the antenna maneuver data.

7. The method of claim 6, wherein:

the generated first portion of the antenna maneuver data identifies a number of satellite antenna maneuvers to be performed in a time period and target azimuth and elevation angles for each of the number of satellite antenna maneuvers; and

the generated second portion of the antenna maneuver data identifies a time at which to perform each of the number of satellite antenna maneuvers.

8. The method of claim 1, wherein computing the satellite antenna maneuver data includes:

defining an ellipse formed on the earth'"'"'s surface by the satellite antenna beam pointing position due to the inclined orbit of the satellite;

segmenting the defined ellipse into a plurality of arcs;

moving each of the plurality of arcs to the nominal satellite antenna beam pointing position on the earth'"'"'s surface; and

determining angular distances from points on each moved arc to the nominal satellite antenna beam pointing position on the earth'"'"'s surface;

wherein the satellite antenna maneuver data is at least in part computed based on the determined angular distances.

9. The method of claim 1, wherein the nominal satellite antenna beam pointing position on the earth'"'"'s surface is a target latitude and target longitude of the satellite antenna beam center on the earth'"'"'s surface.

10. A satellite control center for redirecting a satellite antenna beam from a satellite antenna of an inclined orbit satellite to a nominal satellite antenna beam pointing position on the earth'"'"'s surface, comprising:

an interface configured to receive satellite telemetry, orbital, and antenna nominal pointing information associated with the inclined orbit satellite;

a processor configured to compute satellite antenna maneuver data based upon the received information, and to generate command code sequences corresponding to the generated maneuver data executable at the inclined orbit satellite to modify azimuth and elevation angles of the satellite antenna; and

a transmitter configured to transmit, to the inclined orbit satellite, the generated command code sequences to redirect the satellite antenna beam center close to the nominal satellite antenna beam pointing position on the earth'"'"'s surface.

11. The satellite control center of claim 10, wherein:

the satellite telemetry, orbital, and antenna nominal pointing information includes satellite attitude data, satellite orbit element data, and one of i) the nominal satellite antenna beam pointing position on the earth'"'"'s surface and ii) a nominal satellite antenna beam pointing position on the satellite;

the nominal satellite antenna beam pointing position on the earth'"'"'s surface corresponds to a target latitude and target longitude; and

the nominal satellite antenna beam pointing position on the satellite corresponds to target azimuth and target elevation angles of the satellite antenna.

12. The satellite control center of claim 11, wherein the satellite orbit element data includes a plurality of satellite orbit parameters.

13. The satellite control center of claim 10, wherein the computed satellite antenna maneuver data includes data indicating a number of satellite antenna maneuvers to be performed in a time period, a time at which to perform each of the number of satellite antenna maneuvers, and azimuth and elevation angles for each of the number of satellite antenna maneuvers.

14. The satellite control center of claim 10, wherein the processor if further configured to perform a plurality of coordinate frame transformations to compute the satellite antenna maneuver data.

15. The satellite control center of claim 14, wherein the processor is further configured to, in computing the satellite antenna maneuver data, i) perform an earth station top centric frame to satellite centric frame transformation based upon the nominal satellite antenna beam pointing position on the earth'"'"'s surface and a satellite inclination value of zero to define first parameters, ii) perform a satellite centric frame to earth centric frame transformation based on the defined first parameters and the actual satellite inclination value to define second parameters, iii) perform an earth station top centric frame to satellite centric frame transformation based on the first and second defined parameters and the actual satellite inclination value to generate a first portion of the antenna maneuver data, and iv) perform a satellite centric frame to earth centric frame transformation based upon the first portion of the antenna maneuver data to generate a second portion of the antenna maneuver data.

16. The satellite control center of claim 15, wherein:

the generated first portion of the antenna maneuver data identifies a number of satellite antenna maneuvers to be performed in a time period and target azimuth and elevation angles for each of the number of satellite antenna maneuvers; and

the generated second portion of the antenna maneuver data is a time at which to perform each of the number of satellite antenna maneuvers.

17. The satellite control center of claim 10, wherein:

the processor is further configured to, in computing the satellite antenna maneuver data, i) define an ellipse formed on the earth'"'"'s surface by the satellite antenna beam pointing position due to the inclined orbit of the satellite, ii) segment the defined ellipse into a plurality of arcs, iii) move each of the plurality of arcs to the nominal satellite antenna beam pointing position on the earth'"'"'s surface, and iv) determine angular distances from points on each moved arc to the nominal satellite antenna beam pointing position on the earth'"'"'s surface; and

the satellite antenna maneuver data is at least in part computed based on the determined angular distances.

18. The satellite control center of claim 10, wherein the nominal satellite antenna beam pointing position on the earth'"'"'s surface is a target latitude and target longitude of the satellite antenna beam center on the earth'"'"'s surface.

19. An article of manufacture for redirecting a satellite antenna beam from a satellite antenna of an inclined orbit satellite to a nominal satellite antenna beam pointing position on the earth'"'"'s surface, comprising:

a computer readable medium; and

computer programming stored on the medium;

wherein the stored computer programming is configured to be readable from the computer readable medium by a computer to thereby cause the computer to operate so as to;

receive telemetry, orbital, and antenna nominal pointing information associated with the inclined orbit satellite;

compute satellite antenna maneuver data based upon the received information;

generate command code sequences corresponding to the generated maneuver data executable at the inclined orbit satellite to modify azimuth and elevation angles of the satellite antenna; and

cause the generated command code sequences to be transmitted to the inclined orbit satellite to redirect the satellite antenna beam center close to the nominal satellite antenna beam pointing position on the earth'"'"'s surface.

20. The article of manufacture of claim 19, wherein the computer programming is further configured to perform a plurality of coordinate frame transformations in computing the satellite antenna maneuver data.