Satellite beam steering reference using terrestrial beam steering terminals

• US 5,758,260 A
• Filed: 08/23/1995
• Issued: 05/26/1998
• Est. Priority Date: 08/23/1995
• Status: Expired due to Fees

• Current Assignee: Globalstar Incorporated
• Original Assignee: Globalstar Incorporated
• Inventors: Wiedeman, Robert A.
• Primary Examiner(s): Pham, Chi H.
• Application Number:
  US08/518,524
• Time in Patent Office: 1,007 Days
• Field of Search: 455/12.1, 455/13.1, 455/13.4, 244/164, 342/352, 342/353, 342/354, 342/355, 342/357, 342/358, 342/359, 342/368, 364/434
• US Class Current: 455/12.1
• CPC Class Codes: B64G 1/1007 Communications satellites
• CPC Class Codes: B64G 1/244 Spacecraft control systems
• CPC Class Codes: B64G 1/363 using sun sensors
• CPC Class Codes: B64G 1/365 using horizon or Earth sensors
• CPC Class Codes: B64G 1/366 using magnetometers
• CPC Class Codes: B64G 1/66 Arrangements or adaptations of apparatus or instruments, not otherwise provided for
• CPC Class Codes: B64G 3/00 Observing or tracking cosmonautic vehicles
• CPC Class Codes: H04B 7/2041 Spot beam multiple access

Abstract

A satellite communication system has at least one satellite (1) with an antenna that generates a moving beam pattern on the surface of the earth. The beam pattern (3) is comprised of a plurality of sub-beams (4). A method of this invention determines an attitude correction signal for the satellite by the steps of: (a) providing at least one reference transmitter (10) at a known location on the surface of the earth; (b) transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams; (c) receiving the at least one signal with the satellite antenna and transponding the received at least one signal to a ground station (8). A next step of the method (d) receives the transponded at least one signal with the ground station; (e) determines a gain of the received at least one signal; (f) compares the determined gain to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and (g) and determines a difference between the determined gain and the expected gain to derive a correction signal indicative of an attitude error of the satellite. The method further includes the steps of transmitting the correction signal to the satellite; and correcting the attitude of the satellite in accordance with the correction signal.

Claims

1. In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining an attitude correction signal for the satellite comprising the steps of:

providing at least one reference transmitter at a known location on the surface of the earth;

transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams;

receiving the at least one signal with the satellite antenna and transponding the received at least one signal to a ground station;

receiving the transponded at least one signal with the ground station;

determining a gain of the received at least one signal;

comparing the determined gain to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and

determining a difference between the determined gain and the expected gain to derive a correction signal indicative of an attitude error of the satellite.

2. A method as set forth in claim 1 and further comprising the steps of:

transmitting the correction signal from the ground station to the satellite; and

correcting the attitude of the satellite in accordance with the correction signal.

3. A method as set forth in claim 1 and further comprising the steps of:

transmitting the correction signal from the ground station to a second ground station;

transmitting the correction signal from the second ground station to the satellite; and

correcting the attitude of the satellite in accordance with the correction signal.

4. A method as set forth in claim 1 wherein the step of transmitting includes a step of transmitting a plurality of signals from one reference transmitter.

5. A method as set forth in claim 1 wherein the step of transmitting includes a step of transmitting a plurality of signals from a plurality of reference transmitters.

6. A method as set forth in claim 1 wherein the step of transmitting includes a step of transmitting one signal from individual ones of a plurality of reference transmitters.

7. A method as set forth in claim 1, wherein the satellite has a preferred direction of travel over the surface of the earth, wherein at least one error angle exists such that the satellite travels in an actual direction that differs from the preferred direction, and wherein the step of determining determines an apparent direction of travel that differs from the actual direction of travel by an angle related to a knowledge uncertainty as to the satellite attitude.

8. A method as set forth in claim 1 wherein the correction signal has a value that is a function of a yaw error angle of the satellite, and further comprising the steps of:

transmitting the correction signal to the satellite; and

correcting the attitude of the satellite in accordance with the correction signal by rotating the satellite about the yaw axis so as to reduce a magnitude of the yaw error angle.

9. A method as set forth in claim 1 wherein the correction signal has a value that is a function of at least one axial misalignment error of the satellite, and further comprising the steps of:

transmitting the correction signal to the satellite; and

correcting the at least one axial misalignment error of the satellite in accordance with the correction signal.

10. A method as set forth in claim 1 wherein the correction signal has a value that is a function of at least one axial misalignment error of the satellite antenna, and further comprising the steps of:

transmitting the correction signal to the satellite; and

correcting the at least one axial misalignment error of the satellite antenna in accordance with the correction signal.

11. A method as set forth in claim 1, wherein the step of transmitting at least one signal from the at least one reference transmitter transmits a spread spectrum, code division multiple access signal, wherein the step of transponding the received at least one signal to a ground station transmits the spread spectrum, code division multiple access signal into at least one feeder link channel, and wherein the step of receiving the transponded at least one signal with the ground station receives the transponded spread spectrum, code division multiple access signal from the at least one feeder link channel.

12. In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a satellite attitude correction system comprising:

at least one reference transmitter at a known location on the surface of the earth;

means for transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams;

means for receiving the at least one signal from the satellite antenna and for transponding the received at least one signal to a ground station;

means for receiving the transponded at least one signal with the ground station;

means for determining a gain of the received at least one signal and for comparing the determined gain to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and

means for determining a difference between the determined gain and the expected gain to derive a correction signal indicative of an attitude error of the satellite.

13. The satellite attitude correction system of claim 12, and further comprising:

means for transmitting the correction signal from the ground station to the satellite; and

means in said satellite for correcting the attitude of the satellite in accordance with the correction signal.

14. The satellite attitude correction system of claim 12, and further comprising:

means for transmitting the correction signal from the ground station to a second ground station;

means for transmitting the correction signal from the second ground station to the satellite; and

means in said satellite for correcting the attitude of the satellite in accordance with the correction signal.

15. The satellite attitude correction system of claim 12, wherein said transmitting means transmits a plurality of signals from one reference transmitter.

16. The satellite attitude correction system of claim 12, wherein said transmitting means transmits a plurality of signals from a plurality of reference transmitters.

17. The satellite attitude correction system of claim 12, wherein said transmitting means transmits one signal from individual ones of a plurality of reference transmitters.

18. The satellite attitude correction system of claim 12, wherein the satellite has a preferred direction of travel over the surface of the earth, wherein at least one error angle exists such that the satellite travels in an actual direction that differs from the preferred direction, and wherein said determining means determines an apparent direction of travel that differs from the actual direction of travel by an angle related to a knowledge uncertainty as to the satellite attitude.

19. The satellite attitude correction system of claim 12, wherein the correction signal has a value that is a function of a yaw error angle of the satellite, and further comprising:

means for transmitting the correction signal to the satellite; and

means in said satellite for correcting the attitude of the satellite in accordance with the correction signal by rotating the satellite about the yaw axis so as to reduce a magnitude of the yaw error angle.

20. The satellite attitude error correction system as set forth in claim 12 wherein the correction signal has a value that is a function of at least one axial misalignment error of the satellite, and further comprising:

means for transmitting the correction signal to the satellite; and

means in said satellite for correcting the at least one axial misalignment error of the satellite in accordance with the correction signal.

21. The satellite attitude error correction system as set forth in claim 12 wherein the correction signal has a value that is a function of at least one axial misalignment error of the satellite antenna, and further comprising:

means for transmitting the correction signal to the satellite; and

means in said satellite for correcting the at least one axial misalignment error of the satellite antenna in accordance with the correction signal.

22. The satellite attitude correction system of claim 12, wherein said transmitting means transmits a spread spectrum, code division multiple access signal, wherein said transponding means includes means for transmitting the spread spectrum, code division multiple access signal into at least one feeder link channel, and wherein said ground station includes means for receiving the transponded spread spectrum, code division multiple access signal from the at least one feeder link channel.

23. In a satellite communication system comprising at least one satellite having a steerable antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining an antenna pointing correction signal for the satellite comprising the steps of:

providing at least one reference transmitter at a known location on the surface of the earth;

transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams;

receiving the at least one signal with the satellite antenna and transponding the received at least one signal to a ground station;

receiving the transponded at least one signal with the ground station;

determining a gain of the received at least one signal;

comparing the determined gain to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and

determining a difference between the determined gain and the expected gain to derive a correction signal indicative of a pointing error of the satellite antenna.

24. In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining beam pattern correction signal for the satellite comprising the steps of:

providing at least one reference transmitter at a known location on the surface of the earth;

transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams;

receiving the at least one signal with the satellite antenna;

comparing a gain of the received at least one signal to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and

determining a beam pattern correction signal in accordance with a difference between the actual gain and the expected gain.

25. A method as set forth in claim 24 wherein the step of receiving the at least one signal with the satellite includes a step of retransmitting the received at least one signal;

and wherein the steps of comparing and determining are executed by at least one ground station.

26. A method as set forth in claim 25 and further comprising the steps of:

transmitting the correction signal from the ground station to the satellite; and

correcting the beam pattern in accordance with the correction signal.

27. A method as set forth in claim 25 and further comprising the steps of:

storing the correction;

subsequently transmitting the stored correction signal from the same or a different ground station to the satellite; and

correcting the beam pattern in accordance with the correction signal.

28. A method as set forth in claim 24 wherein the steps of comparing and determining are executed by the satellite.

29. In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining beam pattern correction signal for the satellite comprising the steps of:

providing at least one reference transmitter at a known location on the surface of the earth;

transmitting at least one signal from the at least reference transmitter into at least one of the sub-beams;

receiving the at least one signal with the satellite antenna;

comparing a gain of the received at least one signal to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna;

determining a beam pattern correction signal in accordance with a difference between the actual gain and the expected gain; and

correcting the beam pattern in accordance with the correction signal and in accordance with information obtained from at least one attitude sensor means carried by said satellite.

30. A method as set forth in claim 29 wherein the step of receiving the at least one signal with the satellite includes a step of retransmitting the received at least one signal;

and wherein the steps of comparing and determining are executed by at least one ground station.

31. A method as set forth in claim 30, wherein the step of correcting includes an initial step of transmitting the correction signal from the at least one ground station to the satellite.

32. A method as set forth in claim 30, wherein the step of correcting includes the initial steps of storing the correction signal on the ground;

and subsequently transmitting the correction signal from a ground station to the satellite.

33. In a satellite communication system comprising at least one satellite having an antenna that generates a moving beam pattern on the surface of the earth, the beam pattern being comprised of a plurality of sub-beams, a method for determining beam pattern correction signal for the satellite comprising the steps of:

providing at least one transmitter at a location on the surface of the earth;

transmitting at least one signal from the at least transmitter into at least one of the sub-beams using a predetermined access technique;

receiving the at least one signal with the satellite antenna;

comparing a gain of the received at least one signal to a gain expected to be received based on a predetermined knowledge of a spatial variation in gain of the satellite antenna; and

determining a beam pattern correction signal in accordance with a difference between the actual gain and the expected gain.

34. A method as set forth in claim 33 wherein the predetermined access technique is comprised of a code division, multiple access technique.

35. A method as set forth in claim 33 wherein the predetermined access technique is comprised of a time division, multiple access technique.

36. A method as set forth in claim 33 wherein the predetermined access technique is comprised of a frequency division, multiple access technique.

37. A method as set forth in claim 33 wherein the transmitter forms a portion of a user terminal transceiver.

38. A method as set forth in claim 37 wherein the step of receiving the at least one signal with the satellite includes a step of retransmitting the received at least one signal;

wherein the steps of comparing and determining are executed by at least one ground station that receives the retransmitted signal; and

wherein the at least one ground station is connected to a terrestrial communications system for coupling the user terminal to the terrestrial communications system.