Compact top-loaded, tunable fractal antenna systems for efficient ultrabroadband aircraft operation

• US 7,746,282 B2
• Filed: 05/20/2008
• Issued: 06/29/2010
• Est. Priority Date: 05/20/2008
• Status: Active Grant

• Current Assignee: Sensor Systems
• Original Assignee: Sensor Systems
• Inventors: Lin, Zhen Biao, Lin, Jack J. Q., Robin, Seymour
• Primary Examiner(s): Wimer; Michael C
• Application Number:
  US12/154,209
• Publication Number:
  US 20090289871A1
• Time in Patent Office: 770 Days
• Field of Search: 343/700.MS, 343/752, 343/860, 343/705, 343/745, 343/861, 343/872
• US Class Current: 343/745
• CPC Class Codes: H01Q 1/36 Structural form of radiating elements, e.g. cone, spiral, umbrella; Particular materials used therewithH01Q1/08, H01Q1/14 take precedence
• CPC Class Codes: H01Q 9/36 with top loading
• CPC Class Codes: H01Q 9/40 Element having extended radiating surface

Abstract

Compact top-loaded, fractal monopole antenna system embodiments are provided for multi-band airborne operation over ultrabroadband ranges (e.g., 30 to 2000 MHz). These multi-band embodiments are self-contained, aerodynamic and compact (e.g., blade height less than 9.5 inches) and are power efficient with a low return loss (e.g., less than −7 dB). System embodiments include a set of impedance-matching circuits configured to substantially match an antenna impedance to a predetermined system impedance over a set of predetermined frequency bands. In an embodiment, at least one impedance-matching circuit includes a chain of selectable air-core inductors which are novelly arranged to improve radiation efficiency and prevent damage to support substrates. In an embodiment, a lowest-frequency one of the impedance-matching circuits is configured to process signals having a maximum wavelength λ_max wherein a fractal member is configured with a length that does not exceed λ_max/40. System embodiments are configured to respond to a variety of existing radio systems that send commands via different encoding formats.

Claims

1. An antenna system, comprising:

a conductive fractal member that extends from a first end to a second end and is configured to define an apex at said first end;

a top load having an aerodynamic shape and coupled to said second end; and

an aerodynamically-shaped dielectric blade arranged to surround said fractal member.

2. The system of claim 1, wherein said fractal member is configured to be substantially symmetric about said apex and to define a pattern having self-similar elements.

3. The system of claim 2, wherein said fractal member is configured to define a Sierpinski triangle.

4. The system of claim 1, wherein:

said top load has a diameter and a length sufficient to present a selected capacitance to said fractal member; and

said blade comprises fiberglass.

5. The system of claim 1, further including a set of impedance-matching circuits each selectively coupled to said first end and configured to substantially match an antenna impedance to a predetermined system impedance over a respective one of a set of predetermined frequency bands.

6. The system of claim 1, further including:

a first impedance-matching circuit coupled to said first end and configured to substantially match an antenna impedance to a predetermined system impedance over a predetermined first frequency band; and

a set of impedance-matching circuits each selectively coupled to said first end and configured to substantially match an antenna impedance to a predetermined system impedance over a respective one of a set of predetermined additional frequency bands.

7. The system of claim 6, wherein said first impedance-matching circuit includes a chain of selectable air-core coils to enhance said match over said first frequency band.

8. The system of claim 6, wherein said air-core coils are orthogonally arranged.

9. The system of claim 6, wherein said first impedance-matching circuit is configured to process signals having a maximum wavelength λ

_max and said fractal member is configured with a length between said first and second ends that does not exceed λ

_max/40.

10. The antenna of claim 1, further including a dielectric sheet and wherein said fractal member comprises a copper film on said sheet.

11. An antenna system, comprising:

a conductive member that extends from a first end to a second end;

a top load coupled to add capacitance to said second end; and

a set of impedance-matching circuits each configured to substantially match an antenna impedance at said first end to a predetermined system impedance over a respective one of a set of predetermined frequency bands;

wherein one of said circuits includes a chain of selectable air-core coils to enhance said match over at least one of said frequency bands and further including a support substrate wherein at least two of said air-core coils are orthogonally arranged and supported by and spaced from said substrate.

12. The system of claim 11, wherein at least one of said circuits includes reactance and susceptance elements.

13. The system of claim 11, wherein said conductive member is a fractal member and said top load has an aerodynamic shape.

14. The system of claim 11, wherein a lowest-frequency one of said circuits is configured to process signals having a maximum wavelength λ

_max and said fractal member is configured with a length between said first and second ends that does not exceed λ

_max/40.

15. The system of claim 11, further including:

a transceiver; and

a diplexer coupling said transceiver to said circuits.

16. An antenna system configured to respond to control commands, comprising:

a conductive fractal member that extends from a first end to a second end;

a top load coupled to said second end;

a set of impedance-matching circuits each configured to substantially match a first end impedance to a predetermined system impedance over a respective one of a set of predetermined frequency bands; and

a controller configured to couple any selected one of said circuits to said first end in response to said control commands.

17. The system of claim 16, wherein said controller is further configured to:

determine an identified source of said control commands; and

in accordance with predetermined encoding rules of said identified source, decode said control commands to obtain decoded control commands.

18. The system of claim 17, wherein said controller includes a set of switching diodes arranged to couple respective ones of said circuits to said first end and said controller is configured to turn on selected diodes of said set in response to said decoded control commands.

19. The system of claim 18, wherein said controller includes transistor drivers connected to provide switching currents to said selected diodes in response to said decoded control commands.

20. The system of claim 18, wherein said controller includes a lookup table that identifies said selected diodes in response to said decoded control commands.

21. The system of claim 16, wherein at least one of said circuits includes a chain of selectable air-core coils.

22. The system of claim 21, wherein said air-core coils are orthogonally arranged.

23. The system of claim 16, wherein said top load is configured to define an aerodynamic shape.

24. The system of claim 23, further including an aerodynamically-shaped dielectric enclosure coupled to said top load and arranged to protectively surround said fractal member, said circuits and said controller so that said top load and said enclosure form a self-contained antenna system.