Array fed multiple beam array reflector antenna systems and method

• US 6,392,611 B1
• Filed: 08/17/2000
• Issued: 05/21/2002
• Est. Priority Date: 08/17/2000
• Status: Expired due to Term

• Current Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Original Assignee: Space Systems/Loral Incorporated (Loral Space and Communications Incorporated)
• Inventors: Burr, Douglas G., Hardie, George, Smith, Terry M.
• Primary Examiner(s): Ho, Tan
• Application Number:
  US09/640,936
• Time in Patent Office: 642 Days
• Field of Search: 343/779, 343/781.R, 343/781.CA, 343/781.P, 343/786, 343/840, 343/771, 343/756, 343/909, 343/DIG.2
• US Class Current: 343/912
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 19/195 wherein a reflecting surface acts also as a polarisation filter or a polarising device
• CPC Class Codes: H01Q 25/007 using two or more primary active elements in the focal region of a focusing device for operation on different wavebands H01Q5/22
• CPC Class Codes: H01Q 3/26 varying the relative phase or relative amplitude of energisation between two or more active radiating elements; varying the distribution of energy across a radiating aperture H01Q3/12, H01Q3/22, H01Q3/24 take precedence

Abstract

Array fed multiple beam antenna systems and methods for use on an orbiting spacecraft carrying a communication system. The antenna systems include a reflector and a relatively small array feed compared to the reflector. The array feed has feeds (radiators) that illuminate the reflector and that are disposed in a focal plane of the reflector. A power division network excites the radiators of the feeds. The antenna system is capable of very wide scan angle operation and may be used to provide multiple spot beam coverage over the surface of the Earth viewed from a synchronous orbit spacecraft. Phase aberration normally associated with scanning is corrected by adjusting excitation coefficients of each array feed. The spot beams are scanned across a field of regard by controlling the position of each feed in the focal plane and using the appropriate amplitude and phase distribution associated with a particular spot beam (array feed). The amplitude and phase distributions may be fixed or varied during operation. A dual band system includes a second array feed and a frequency selective surface disposed between the array feeds that optimizes the respective array feeds. Use of the frequency selective surface in dual band implementations produces a very efficient communication system.

Claims

1. A dual band antenna system use on a spacecraft having a communication system comprising:

a reflector;

a first two-dimensional array feed that is relatively small compared to the size of the reflector;

a second two-dimensional array feed that is relatively small compared to the size of the reflector;

a power division network coupled between the communication system and the first and second array feeds; and

a frequency selective surface disposed between the first and second array feeds.

2. The antenna system recited in claim 1 wherein the array feed comprises a plurality of feeds that illuminate the reflector.

3. The antenna system recited in claim 2 wherein the each of the feeds comprises a plurality of radiators.

4. The antenna system recited in claim 3 wherein the power division network excites each of the radiators of the feeds.

5. The antenna system recited in claim 3 wherein the radiators of each the feeds are arranged in a square grid pattern.

6. The antenna system recited in claim 3 wherein the radiators of each the feeds are arranged in a rectangular grid pattern.

7. The antenna system recited in claim 3 wherein the radiators of each the feeds are arranged in a triangular grid pattern.

8. The antenna system recited in claim 3 wherein the radiators of each the feeds are disposed in a focal plane of the reflector.

9. The antenna system recited in claim 1 wherein the feed array comprises a waveguide slot array.

10. The antenna system recited in claim 1 wherein the reflector comprises an offset reflector.

11. The antenna system recited in claim 1 wherein spot beams are scanned across a field of regard by appropriate positioning if the feed array in the focal plane and the sidelobes of each beam are optimized for interbeam isolation by controlling amplitude and phase distributions associated with each array feed.

12. The antenna system recited in claim 1 wherein amplitude and phase distributions associated with each array feed are fixed.

13. The antenna system recited in claim 1 wherein amplitude and phase distributions associated with each array feed are variable.

14. A method of Generating multiple spot beams comprising the steps of:

launching a spacecraft into orbit that carries a communication system having a multiple beam antenna system including a reflector and first and second two-dimensional array feeds each having a plurality of radiators that are coupled to the communication system by way of a power division network, and a frequency selective surface disposed between the first and second array feeds;

during transmission, coupling RF energy from the communication system by way of the power division network to the radiators of the respective feeds of one of the two-dimensional array feeds to excite each of the radiators thereof;

reflecting energy radiated by the radiators of the one of the two-dimensional array feeds from the reflector to produce multiple spot beams;

during reception, reflecting the multiple spot beams from the reflector to the radiators of the feeds of the other two-dimensional array feed using the frequency selective surface; and

coupling the RF energy contained in the multiple spot beams by way of the power division network to the communication system.

15. The method recited in claim 14 wherein spot beams are scanned across a field of regard by array position, and performance is optimized by controlling amplitude and phase distributions associated with each array feed.

16. The method recited in claim 14 wherein amplitude and phase distributions associated with each array feed are fixed.

17. The method recited in claim 14 wherein amplitude and phase distributions associated with each array feed are variable.

18. The method recited in claim 14 wherein the amplitude and phase distributions produced by the radiators are controlled to produce different beam distributions for different scan positions to optimize beamshapes generated by the multiple beam antenna system over a very wide coverage region.