Antenna assembly and a method for satellite tracking

• US 7,492,323 B2
• Filed: 10/19/2005
• Issued: 02/17/2009
• Est. Priority Date: 11/04/2004
• Status: Expired due to Fees

• Current Assignee: Spacecom Holding ApS
• Original Assignee: Spacecom Holding ApS
• Inventors: Nielsen, Peter
• Primary Examiner(s): Ho; Tan
• Application Number:
  US11/718,558
• Publication Number:
  US 20070290936A1
• Time in Patent Office: 1,217 Days
• Field of Search: 343/757, 343/758, 343/765, 343/766, 343/781.CA, 343/840, 342/359
• US Class Current: 343/757
• CPC Class Codes: H01Q 1/125 Means for positioning
• CPC Class Codes: H01Q 1/18 Means for stabilising antennas on an unstable platform
• CPC Class Codes: H01Q 21/28 Combinations of substantially independent non-interacting antenna units or systems multiple beam H01Q25/00
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation

Abstract

The present invention relates to a method for satellite tracking by use of an antenna assembly having a master antenna for receiving and transmitting signals to and from a master antenna satellite in a first frequency band, and a slave antenna for receiving signals from a slave antenna satellite in a second satellite band, where the master and slave antennas have physical bore-sight axes which can be arranged at different directions in relation to each other. The method of the invention includes a master antenna search routine and a slave antenna search routine. The master antenna search routine comprises the steps of changing or switching a direction of reception of the master antenna, monitoring, during the changing or switching of direction of reception of the master antenna. The slave antenna search routine comprises the steps of arranging the direction of the physical bore-sight axis of the slave antenna at a first slave direction, where the first slave direction is at least partly based on the obtained direction of the physical bore-sight axis of the master antenna.

Claims

1. An antenna assembly for satellite tracking, said antenna assembly comprising:

a master antenna for receiving and transmitting first satellite signals to and from a master antenna satellite in a first frequency band,

a slave antenna for receiving second satellite signals from a slave antenna satellite in a second satellite band, said master and slave antennas being mounted on the same stabilizing platform,

a master drive assembly for mechanically changing the direction of a physical bore-sight axis of the master antenna, and

a slave drive assembly for mechanically changing the direction of a physical bore-sight axis of the slave antenna,

wherein said master and slave assemblies are adapted for arranging the physical bore-sight axes of the master antenna and the slave antenna at different directions in relation to each other in response to one or more master-slave control signals,

wherein the antenna assembly further comprises control means for providing one or more master-slave control signals to the slave drive assembly to thereby control the arrangement of the direction of the physical bore-sight axis of the slave antenna in relation to the physical bore-sight axis of the master antenna so that the angular distance in azimuth between said physical bore-sight axes is set at a given azimuth value, ALPHA(AZ), and

wherein the control means for providing the one or more master-slave controls signals to the slave drive assembly is further adapted for providing control signals to thereby control the arrangement of the direction of the physical bore-sight axis of the slave antenna so that the angular distance in elevation between the physical bore-sight axis of the slave antenna and the horizontal plane is set at a given elevation value, ALPHA(ELS).

2. An antenna assembly according to claim 1, wherein the master antenna is mounted on the slave antenna with the slave antenna being mounted to the stabilizing platform.

3. An antenna assembly according to claim 1, wherein the slave antenna is further adapted for transmitting second satellite signals to the slave antenna satellite in the second satellite band.

4. An antenna assembly according to claim 1, wherein the master antenna is movably secured to the master drive assembly, and the slave antenna is movably secured to the slave drive assembly.

5. An antenna assembly according to claim 1, wherein the master drive assembly is rigidly fixed in relation to the slave antenna.

6. An antenna assembly according to claim 5, further comprising one or more control systems being adapted for providing control signals to the master and slave dive assemblies in order to lock the physical bore-sight axes of the master antenna and the slave antenna in the same vertical plane, whereby when mechanically moving the master antenna to change the direction in azimuth of the physical bore-sight axis of the master antenna, the direction of the physical bore-sight axis of the slave antenna is mechanically changed to the same degree in azimuth.

7. An antenna assembly according to claim 1, further comprising master antenna switching means for changing or switching a direction of reception of the master antenna.

8. An antenna assembly according to claim 7, wherein the master antenna switching means is adapted for performing a mechanically changing or switching of the direction of the physical bore-sight axis of the master antenna followed by an electrically changing or switching of the direction of reception of the master antenna.

9. An antenna assembly according to claim 8, wherein the master antenna is an array antenna.

10. An antenna assembly according to claim 9, wherein the master antenna switching means is adapted for performing the electrically changing or switching of the direction of reception of the master antenna by use of beam switching or beam squint technology.

11. An antenna assembly according to claim 7, further comprising monitor means for monitoring, during the changing or switching of direction of reception of the master antenna, one or more signals carrying information representing variations in receiving signal strength of one or more signals transmitted from the master antenna satellite.

12. An antenna assembly according to claim 11, further comprising control means for providing one or more master control signals to the master drive assembly and/or the slave drive assembly to thereby control the movement of the master antenna in response to the results of the monitoring of the signal strength information signal(s) corresponding to the signal(s) from the master antenna satellite, thereby changing the direction of the physical bore-sight axis of the master antenna so as to reduce pointing errors of the master antenna in relation to the master antenna satellite.

13. An antenna assembly according to claim 1, further comprising slave antenna switching means for changing or switching a direction of reception of the slave antenna.

14. An antenna assembly according to claim 13, wherein the slave antenna switching means is adapted for performing a mechanically changing or switching of the direction of the physical bore-sight axis of the slave antenna.

15. An antenna assembly according to claim 13, further comprising monitor means for monitoring, during the changing or switching of direction of reception of the slave antenna, one or more signals carrying information representing variations in receiving signal strength of one or more signals transmitted from the slave antenna satellite.

16. An antenna assembly according to claim 15, further comprising control means for providing one or more slave control signals to the slave drive assembly and/or the master drive assembly to thereby control the movement of the slave antenna in response to the results of the monitoring of the signal strength information signal(s) corresponding to the signal(s) from the slave antenna satellite, thereby changing the direction of the physical bore-sight axis of the slave antenna so as to reduce pointing errors of the slave antenna in relation to the slave antenna satellite.

17. An antenna assembly according to claim 1, wherein the slave antenna comprises a main reflector for reflecting said slave antenna satellite signals and a feed unit for receiving the reflected slave antenna satellite signals, said slave antenna being of the Cassegrain type having a sub-reflector arranged substantially inside the focus of the main reflector and having the feed unit arranged substantially at the surface of the main reflector, and wherein the master drive assembly is arranged at least partly at a blind spot of the slave antenna in front of the sub-reflector.

18. A method for satellite tracking by use of an antenna assembly having a master antenna for receiving and transmitting first satellite signals to and from a master antenna satellite in a first frequency band, and a slave antenna for receiving second satellite signals from a slave antenna satellite in a second frequency band, said master and slave antennas being mounted on the same stabilizing platform and having physical bore-sight axes which can be arranged at different directions in relation to each other, said method including:

a) a master antenna search routine comprising the steps of;

changing or switching a direction of reception of the master antenna,

monitoring, during the changing or switching of direction of reception of the master antenna, one or more signals carrying information representing variations in receiving signal strength of one or more signals transmitted from the master antenna satellite, and

mechanically moving the master antenna in response to the results of the monitoring of the signal strength information signal(s) corresponding to the signal(s) from the master antenna satellite, thereby obtaining a direction of the physical bore-sight axis of the master antenna resulting in reduced pointing errors of the master antenna in relation to the master antenna satellite; and

b) a slave antenna search routine comprising the steps of;

arranging the direction of the physical bore-sight axis of the slave antenna at a first slave direction,

wherein the arrangement of the direction of the physical bore-sight axis of the slave antenna at the first slave direction comprises arranging the angular distance in azimuth between the physical bore-sight axes of the master antenna and the slave antenna at a given azimuth value, and

wherein the arrangement of the direction of the physical bore-sight axis of the slave antenna at the first slave direction further comprises arranging the angular distance in elevation between the physical bore-sight axis of the slave antenna and the horizontal plane at a given elevation value, ALPHA(ELS),

said given azimuth value and said given elevation value being determined from the obtained direction of the physical bore-sight axis of the master antenna, the orbital position of the master antenna satellite, the orbital position of the slave antenna satellite, and the geographical position of the antenna assembly.

19. A method according to claim 18, wherein the master antenna is mounted on the slave antenna with the slave antenna being mounted to the stabilizing platform.

20. A method according to claim 18, wherein after the arrangement of the physical bore-sight axis of the slave antenna at the first slave direction, the slave antenna search routine further comprises:

changing or switching a direction of reception of the slave antenna,

monitoring, during the changing or switching of direction of reception of the slave antenna, one or more signals carrying information representing variations in receiving signal strength of one or more signals transmitted from the slave antenna satellite, and

mechanically moving the slave antenna in response to the results of the monitoring of the signal strength information signal(s) corresponding to the signal(s) from the slave antenna satellite, thereby changing the direction of a physical bore-sight axis of the slave antenna so as to reduce pointing errors of the slave antenna in relation to the slave antenna satellite.

21. A method according to claim 18, said method further including an initial setting routine being performed before the master antenna search routine, said initial setting routine comprising:

locking the physical bore-sight axes of the master antenna and the slave antenna in the same vertical plane, whereby when mechanically moving the master antenna to change the direction in azimuth of the physical bore-sight axis of the master antenna, the direction of the physical bore-sight axis of the slave antenna is mechanically changed to the same degree in azimuth, said locking being maintained during the master search routine.

22. A method according to claim 21, wherein the initial setting routine comprises arranging and maintaining the physical bore-sight axis of the slave antenna at a substantially horizontal position.

23. A method according to claim 22, wherein the initial setting routine further comprises arranging and maintaining the physical bore-sight axis of the master antenna at a substantially horizontal position.

24. A method according to claim 18, wherein the changing or switching of the direction of reception of the master antenna in the master antenna search routine comprises a mechanically changing or switching of the direction of the physical bore-sight axis of the master antenna followed by an electrically changing or switching of the direction of reception of the master antenna.

25. A method according to claim 24, wherein the electrically changing or switching of the direction of reception of the master antenna is initiated when one or more signals transmitted from the master antenna satellite are received by a given signal strength.