Electronically scanned antenna

• US 4,074,268 A
• Filed: 06/21/1976
• Issued: 02/14/1978
• Est. Priority Date: 06/21/1976
• Status: Expired due to Term

• Current Assignee: NavCom Defense Electronics, Inc. (Transdigm Group Incorporated)
• Original Assignee: Hoffman Electronics Corporation
• Inventors: Olson, Roy H.
• Primary Examiner(s): Wilbur, Maynard R.
• Assistant Examiner(s): Berger, Richard E.
• Application Number:
  US05/697,868
• Time in Patent Office: 603 Days
• Field of Search: 343/106 R, 343/854
• US Class Current: 342/399
• CPC Class Codes: H01Q 3/28 varying the amplitude
• CPC Class Codes: H01Q 3/46 Active lenses or reflecting arrays
• CPC Class Codes: H01Q 9/40 Element having extended radiating surface

Abstract

There is disclosed herein an antenna for generating a rotating pattern. The pattern is generated electronically, and no physically moving parts are required. An exemplary embodiment of the antenna radiates a cardioid pattern which rotates at a 15Hz rate for use as a Tacan beacon. The structure of the antenna is in the form of a conic monopole above a ground plane. A plurality of vertical modulator fins, providing controllable shorting elements, and a plurality of suppressor posts are added. The modulator fins have associated diodes to which are applied a bias current along with modulating signals which cause the resistance of the diodes to vary with respect to the flow of RF current at the frequencies of interest (such as in the neighborhood of 1 GHz for Tacan usage). Other details of the physical structure of the antenna are shown and described herein, as well as an electronic system for controlling the diodes. In a typical application, the antenna is mounted on an airplane to enable the airplane to serve as a beacon. In this instance, the exemplary system as shown and described herein is adapted to be coupled with the synchro system of the airplane compass for providing a reference with respect to magnetic north so as to properly electronically relate the rotating pattern of the antenna to magnetic north while the airplane upon which the antenna is mounted changes its flight direction.

Claims

1. An antenna for electronically generating a rotating radiation pattern comprising

conic means for radiating electro-magnetic energy,

baseplate means forming a ground plane, said conic means forming a conic monopole and being mounted above said ground plane,

a plurality of modulator fin means disposed between said baseplate means and said conic means for altering the pattern of radiation radiated by said conic means, said modulator fin means including controllable variable resistance means electrically connected to said conic means, and

electrical circuit means coupled with said controllable variable resistive means for causing a predetermined out-of-phase change in the resistance of said variable resistive means of at least two of said modulator fin means.

2. An antenna as in claim 1 including

suppressor means electrically connected between said conic means and said baseplate means for suppressing portions of the pattern of radiation.

3. An antenna as in claim 1 wherein

said modulator fin means comprise four modulator fin means symmetrically arranged 90°

apart, and

suppressor means are symmetrically disposed between said modulator fin means and are electrically connected between said conic means and said baseplate means.

4. An antenna as in claim 3 wherein

said controllable variable resistive means each comprises PIN diode means, and

said electrical circuit means comprises an electrical circuit for applying out-of-phase currents to respective pairs of said diode means.

5. An antenna as in claim 1 wherein

each of said modulator fin means is electrically connected to said baseplate means by respective capacitor means, said capacitor means being formed of metal plates separated from said baseplate means by a dielectric.

6. An antenna as in claim 5 including

a plurality of electro-magnetic energy bypass capacitors, said capacitors being formed of metal plates separated from the underside of said baseplate means by a dielectric, and

means electrically connecting the variable resistive means of said fin means to said bypass capacitors.

7. An antenna as in claim 1 wherein

said modulator fin means comprise four modulator fins disposed on 90°

radials with respect to said baseplate means and said conic means,

said electrical circuit means comprises a circuit for generating four 90°

out-of-phase signals and includes means for applying said signals to the variable resistance means of the respective four modulator fins and for applying a predetermined bias to said variable resistance means, and

suppressor means symmetrically disposed between said modulator fins electrically connected between said conic means and said baseplate means.

8. An antenna as in claim 7 wherein

said electrical circuit means comprises oscillator means coupled with phase generator means, said phase generator means providing a reference signal and a 90°

lagging signal, and said circuit means comprising amplifiers responsive to said reference signal and said lagging signal for generating said four 90°

out-of-phase signals.

9. An antenna as in claim 1 wherein

said electrical circuit means comprises clock means and phase generator means for generating a reference signal and a 90°

lagging signal from which modulating signals are derived for causing the predetermined out-of-phase change in the resistance of said variable resistive means, and

said circuit means further includes means responsive to signals from a magnetic compass and responsive to said reference and lagging signals for generating a control signal which is a function of a compass heading signal related to the pattern generated by said antenna.

10. An antenna for electronically generating a rotating radiation pattern comprising

conic means for radiating electro-magnetic energy,

baseplate means forming a ground plane, said conic means forming a conic monopole and being mounted above said ground plane,

a plurality of modulator fin means disposed between said baseplate means and said conic means for altering the pattern of radiation radiated by said conic means, said modulator fin means including controllable resistance means electrically connected to said conic means,

a plurality of suppressor means symmetrically disposed between said modulator fin means,

said supressor means being electrically connected between said conic means and said baseplate means for suppressing portions of said pattern of radiation, and

electrical circuit means coupled with said controllable resistive means for causing a predetermined out-of-phase change in the resistance of said variable resistive means of at least two of said modulator fin means.

11. An antenna as in claim 10 wherein

said modulator fin means comprise four modulator fin means symmetrically arranged 90°

apart, and

said controllable resistive means each comprises diode means, and

said electrical circuit means comprises an electrical circuit for supplying out-of-phase currents to respective pairs of said diode means.

12. An antenna as in claim 10 wherein

said modulator fin means comprise at least four modulator fin disposed symmetrically on radials with respect to said baseplate means and said conic means, and

said electrical circuit means comprises a circuit for generating at least four out-of-phase signals and includes means for applying said signals to the controllable resistance means of the respective modulator fins and for applying a predetermined bias to said resistance means.

13. An antenna as in claim 10 wherein

said electrical circuit means comprises clock means for generating control signals from which modulating signals are derived for causing the predetermined out-of-phase change in the resistance of said controllable resistive means, and

said circuit means includes means responsive to signals from a magnetic compass and responsive to said control signals for generating a signal which is a function of a compass heading signal related to the pattern generated by said antenna.

14. A Tacan antenna for electronically generating a rotating 15Hz radiation pattern comprising

conic means for radiating electro-magnetic energy,

baseplate means forming a ground plane, said conic means forming a conic monopole and being mounted above said ground plane,

at least four modulator fin means symmetrically disposed between said baseplate means and said conic means for altering the pattern of radiation radiated by said conic means, said modulator fin means including variable resistance means electrically connected to said conic means, said variable resistive means each comprising diode means,

at least four suppressor means symmetrically disposed between said modulator fin means, said suppressor means being electrically connected between said conic means and said baseplate means for suppressing portions of the pattern of radiation, and

electrical circuit means coupled with said controllable variable resistive means for causing a predetermined out-of-phase change in the resistance of said variable resistive means of said modulator fin means, said electrical circuit means comprising an electrical circuit for supplying out-of-phase currents to respective pairs of said diode means.

15. An antenna as in claim 14 wherein

each of said modulator fin means is electrically connected to said baseplate means by respective capacitor means, said capacitor means being formed of metal plates separated from said baseplate means by a dielectric,

a plurality of electro-magnetic bypass capacitors, said capacitors being formed of metal plates separated from the underside of said baseplate means by a dielectric,

means electrically connecting the variable resistive means of said fin means to said bypass capacitors,

said modulator fin means comprise four modulator fins diposed on 90°

radials with respect to said baseplate means and said conic means, and

said electrical circuit means comprises a circuit for generating four 90°

out-of-phase signals and includes means for applying said signals to the variable resistance means of the respective four modulator fins and for applying a predetermined bias to said variable resistance means.

16. An antenna as in claim 15 wherein

said electrical circuit means comprises means for generating a reference signal and a 90°

lagging signal from which modulating signals are derived for causing the predetermined out-of-phase change in the resistance of said variable resistive means, and

said circuit means includes means responsive to signals from a magnetic compass and responsive to said reference and lagging signals for generating a Tacan north burst trigger control signal which is a function of a compass heading signal related to the pattern generated by said antenna.

17. A system for controlling the generation of a heading reference signal from an antenna mounted on an aircraft, which antenna electronically generates a rotating radiation pattern and wherein the antenna includes means for developing said pattern and wherein the system develops an electrical relationship between signals from a magnetic compass of the aircraft and the pattern generated by the antenna, comprising

means coupled with the magnetic compass for translating space equivalent three-phase signals thereof to two-phase equivalent signals,

means for storing the two-phase equivalent signals,

generating means for generating control signals, and means responsive to the control signals for controlling the rotating pattern of the antenna,

circuit means responsive to said control signals for modulating the stored signal as a function of radiation pattern rotation, and for developing signals defining the compass heading phase angle relationship synchronized with said radiation pattern rotation, and

means responsive to said circuit means for generating said heading reference signal.

18. A system for electronically relating the rotating pattern of an antenna to a predetermined compass heading wherein the antenna and compass are adapted to be mounted on an object which changes direction, and wherein the compass includes a compass synchro transmitter and the antenna electronically generates a rotating radiation pattern, comprising

combining means for combining signals from the compass synchro transmitter and for performing a coordinate translation from space equivalent three-phase signals of the compass synchro system to a two-phase equivalent,

means responsive to said combining means for storing signals having a relative polarity and magnitude proportional to the relationship of the predetermined compass heading to a point on the object,

switching means for modulating the stored signals into signals of predetermined frequency and phase relationship which are synchronously time related to the pattern generated by the antenna and for yielding the signal waves representing the compass heading phase angle relationship synchronized with antenna pattern rotation, and

combining means for receiving said signal waves and generating a predetermined reference signal related to said predetermined compass heading.

19. A system as in claim 20 wherein

said object is an aircraft, said antenna generates a 15Hz Tacan radiation pattern, said compass synchro transmitter provides four signals which are combined by said combining means, and said predetermined compass heading is magnetic north and the point on the object represents the nose of the aircraft,

the compass synchro transmitter receives an alternating current reference, and the storage means stores signals at each positive peak of said alternating current reference,

said switching means receives 90°

out-of-phase 15Hz switching signals, and

said predetermined reference signal generated is a Tacan north burst trigger control signal.