Antenna system for satellite digital audio radio service (DARS) system

• US 6,002,359 A
• Filed: 06/13/1997
• Issued: 12/14/1999
• Est. Priority Date: 06/13/1997
• Status: Expired due to Term

• Current Assignee: Northrop Grumman Systems Corporation (Northrop Grumman Corporation)
• Original Assignee: TRW Inc. (Northrop Grumman Corporation)
• Inventors: Chen, Chun-Hong Harry
• Primary Examiner(s): Blum, Theodore M.
• Application Number:
  US08/874,743
• Time in Patent Office: 914 Days
• Field of Search: 342/352, 342/354, 373/895, 373/767, 373/770, 373/771
• US Class Current: 342/352
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 11/08 Helical antennas
• CPC Class Codes: H01Q 13/22 Longitudinal slot in boundary wall of waveguide or transmission line H01Q13/203 takes precedence
• CPC Class Codes: H01Q 15/244 converting a linear polarised wave into a circular polarised wave guided wave H01P1/17
• CPC Class Codes: H01Q 21/005 Slotted waveguides arrays

Abstract

A digital audio radio service (DARS) antenna system is provided. The DARS antenna system includes a broadcast antenna mounted on a spacecraft. The broadcast antenna includes a slotted waveguide direct radiating array (SWDRA). The DARS antenna system also includes a mobile user receive antenna having a quadrifilar helix antenna (QHA). The DARS antenna system further includes a parallel plate polarizer arranged on the broadcast antenna for generating circular polarization. In an embodiment, the polarizer has a plurality of thin plates arranged perpendicular to the SWDRA surface. Broadcast antenna is optimized for overall system performance and is capable of high RF power and beam shaping. The DARS antenna system is also highly reliable and easily deployed from a spacecraft. An embodiment of the DARS antenna system of the present invention further includes "universal" model and "regional" model mobile antennas to easily accommodate personal travel and commuter needs.

Claims

1. A digital audio radio service (DARS) antenna system comprising:

a broadcast antenna mounted on a spacecraft, the broadcast antenna including a slotted waveguide direct radiating array (SWDRA); and

a mobile user receive antenna including a quadrifilar helix antenna (QHA).

2. The DARS antenna system of claim 1 further comprising:

a parallel plate polarizer arranged on the broadcast antenna for generating circular polarization (CP).

3. The DARS antenna system of claim 2 wherein the parallel plate polarizer comprises a plurality of thin plates arranged perpendicular to the SWDRA surface.

4. The DARS antenna system of claim 1 wherein the broadcast antenna transmits at a power level of approximately 1.5 kilowatts.

5. The DARS antenna system of claim 1 wherein the broadcast antenna shapes a transmit beam to approximate a shape of a broadcast area.

6. The DARS antenna system of claim 1 wherein the DARS antenna system operates in the S-band between 2,320 MHz and 2,345 MHz.

7. The DARS antenna system of claim 1 wherein the DARS antenna system provides digital audio from at least two geosynchronous orbit slots.

8. The DARS antenna system of claim 1 wherein the broadcast antenna has adjustable phase.

9. The DARS antenna system of claim 1 wherein the broadcast antenna has adjustable aperture amplitude.

10. The DARS antenna system of claim 1 wherein the broadcast antenna has high thermal and electrical conductivity.

11. The DARS antenna system of claim 1 wherein the broadcast antenna is constructed in aluminum.

12. The DARS antenna system of claim 1 wherein the broadcast antenna is constructed in a metalized composite material.

13. The DARS antenna system of claim 1 further comprising:

a rotation mechanism to deploy the broadcast antenna on orbit from the spacecraft.

14. The DARS antenna system of claim 13 wherein the rotation mechanism comprises a torsion spring.

15. The DARS antenna system of claim 1 wherein the SWDRA further comprises:

a first plurality of subarrays each having a second plurality of slots cut in walls of a third plurality of waveguides.

16. The SWDRA of claim 15 wherein the first plurality is 32, the second plurality is five and the third plurality is five.

17. The DARS antenna system of claim 15 further comprising:

a waveguide network of branchline couplers connecting the first plurality of subarrays.

18. The DARS antenna system of claim 1 further comprising:

a printed circuit QHA having four identical helical windings equally spaced on a cylindrical surface.

19. The DARS antenna system of claim 18 further comprising:

a microstrip balun feeding the four for helical windings equally in amplitude and with 90°

phase progression, the four helical windings and the balun fabricated on a single thin dielectric circuit sheet using standard photo-etching printed circuit processing techniques.

20. The DARS antenna system of claim 19 wherein the circuit sheet is wrapped around a tube.

21. The DARS antenna system of claim 1 wherein the QHA is approximately four inches long and 0.4 inches in diameter.

22. The DARS antenna system of claim 1 wherein the QHA is self-polarizing.

23. The DARS antenna system of claim 1 wherein the mobile antenna has an antenna pattern shaped to peak gain between 20°

and 80°

from zenith.

24. The DARS antenna system of claim 1 wherein the mobile antenna is azimuthally omni-directional.

25. The DARS antenna system of claim 1 further comprising:

integrated front-end LNA directly into a mobile antenna base.

26. The DARS antenna system of claim 1 further comprising:

a universal model of the mobile antenna favoring low elevation angles and providing reception from elevational angles of 70°

-10°

.

27. The DARS antenna system of claim 1 further comprising a regional model of the mobile antenna having a relatively higher gain at a preselected range of elevation angles.

28. The DARS antenna system of claim 1 wherein the mobile antenna is removable and replaceable.