Claims
- 1. A circular directional array antenna comprising:
a driven omnidirectional traveling-wave antenna element coupled to a transceiver via a feed network; and a plurality of surface-waveguide elements symmetrically positioned about and concentrically spaced from the driven omnidirectional traveling-wave antenna element, each surface-waveguide element configured to receive a control signal configured to alter a surface-waveguide transmission characteristic.
- 2. The circular directional array antenna of claim 1, further comprising:
a ground plane having a plurality of vias, wherein the driven element and the surface-waveguide elements are adjacent to the ground plane and connected to the transceiver and control signal, respectively, through the corresponding feed network and the vias.
- 3. The circular directional array antenna of claim 2, wherein the ground plane comprises a reactive surface.
- 4. The circular directional array antenna of claim 2, wherein the ground plane comprises a conductive surface.
- 5. The circular directional array antenna of claim 2, wherein the ground plane is finite and symmetrical about the driven element.
- 6. The circular directional array antenna of claim 2, wherein the driven omnidirectional traveling-wave antenna element generates an omnidirectional surface wave substantially parallel to the ground plane.
- 7. The circular directional array antenna of claim 2, wherein the ground plane comprises a reactive surface which modifies the shape of the radiation pattern in elevation with respect to the ground plane.
- 8. The circular directional array antenna of claim 1, wherein the driven omnidirectional traveling-wave antenna element comprises a mode-0 slow-wave antenna.
- 9. The circular directional array antenna of claim 1, wherein the driven omnidirectional traveling-wave antenna element comprises a mode-0 spiral-mode microstrip antenna.
- 10. The circular directional array antenna of claim 1, further comprising:
a switching circuit having a plurality of inputs and a corresponding plurality of outputs, the outputs independently responsive to a beam steering means coupled to the inputs, wherein a respective output is coupled to each of the surface-waveguide elements.
- 11. The circular directional antenna of claim 10, wherein the waveguide characteristic of each of the surface-waveguide elements is selectively controlled to pass or reflect a traveling wave.
- 12. The circular directional array antenna of claim 10, comprising:
a conducting enclosure configured to surround the switching circuit to suppress radio frequency leakage and electromagnetic coupling between the driven omnidirectional traveling-wave antenna element and the surface-waveguide elements through the control circuit.
- 13. The circular directional array antenna of claim 12, wherein the conducting enclosure comprises mode suppressors arranged around the switching circuit with a distance between adjacent mode suppressors being less than λ/4, where λ is the wavelength of the highest operating frequency.
- 14. A method for operating a broadband/multiband beam-steered circular array antenna, comprising:
locating a driven broadband/multiband traveling wave antenna element that generates an omnidirectional electromagnetic radiation pattern on a ground plane; concentrically arranging a plurality of broadband/multiband surface-waveguide elements around the driven omnidirectional traveling-wave antenna; and applying control signals configured to steer the electromagnetic radiation by selectively altering waveguide characteristics of respective surface-waveguide elements that receive the control signals.
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application claims priority to copending U.S. provisional application entitled, “Broadband/Multiband Circular Array Antenna,” having Ser. No. 60/480,384, filed Jun. 20, 2003, which is entirely incorporated herein by reference.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0002] The U.S. government has a paid-up license in this invention and the right in limited circumstances to require the patent owner to license others on reasonable terms as provided for by the terms of F04611-01-C-0008 awarded by the Air Force Flight Test Center, Edwards AFB, California 93524.
Provisional Applications (1)
|
Number |
Date |
Country |
|
60480384 |
Jun 2003 |
US |