Monopulse cavity-backed multipole antenna system

• US 4,649,391 A
• Filed: 02/01/1984
• Issued: 03/10/1987
• Est. Priority Date: 02/01/1984
• Status: Expired due to Term

• Current Assignee: Hughes Electronics Corporation (AT&T, Inc.)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Tsuda, George I., Edelsohn, Charles R.
• Primary Examiner(s): Tubbesing, T. H.
• Assistant Examiner(s): Barron, Jr., Gilberto
• Application Number:
  US06/576,078
• Time in Patent Office: 1,133 Days
• Field of Search: 343/16 M, 343/363, 343/364, 343/365, 343/366, 343/427, 343/447, 343/895, 343/784, 343/797, 343/816, 343/795, 343/799
• US Class Current: 342/153
• CPC Class Codes: H01Q 13/18 the slot being backed by, or formed in boundary wall of, a resonant cavity longitudinally slotted cylinder H01Q13/12 ; Open cavity antennas
• CPC Class Codes: H01Q 25/02 providing sum and difference patterns H01Q25/04 takes precedence

Abstract

A cylindrical cavity-backed multipole antenna system for high frequency applications is disclosed. The antenna system comprises a plurality N of planar radiation elements disposed on a dielectric disc mounted on the top surface of a conductive cylindrical cavity and equally spaced about its axis. A network circuit is adapted to introduce, for the system sum signal, progressive phase shifts of 360°/N to signals associated with adjacent elements and, for the difference signal, progressive phase shifts of 720°/N. The antenna system may be used to both transmit and receive electromagnetic radiation. The antenna sum and difference patterns are substantially symmetric in space about the antenna boresight.

Claims

1. An antenna system comprising:

a substantially cylindrical cavity defined by a conductive enclosure and having a center axis;

N radiation elements comprising substantially identical, substantially planar, non-interleaved elements of a polygon shape arranged in a closely packed, substantially symmetrical configuration about the axis of said cavity and adapted for communicating right circularly polarized (RCP) and left circularly polarized (LCP) electromagnetic energy wherein N is no less than six; and

difference signal means coupled thereto for providing an antenna system difference pattern characterized by substantial symmetry in space about the antenna boresight.

2. The antenna system of claim 1 wherein said difference signal means is adapted to provide one difference (RCP) signal for RCP radiation and another difference LCP signal for LCP radiation.

3. The antenna system of claim 2 wherein said difference signal means comprises network circuit means coupled to said radiation elements, said circuit means arranged to couple signals between said elements and a difference RCP network port and a difference LCP network port.

4. The antenna system of claim 3 wherein said network circuit means is further adapted to progressively phase shift signals associated with each element by 720°

/N with respect to the signal associated with adjacent elements.

5. The antenna system of claim 1 wherein said cavity has a depth of approximately 25% of the wavelength at the mid-band frequency of the antenna system frequency band.

6. The antenna system of claim 1 wherein said cavity has a diameter greater than 50% of the wavelength of the lower band-edge frequency of the antenna system frequency band.

7. The antenna system of claim 6 wherein said cavity diameter is approximately 75% of said wavelength.

8. The antenna system of claim 3 wherein said network circuit means includes N coaxial transmission lines fed through openings in said enclosure, each having an inner conductor coupled to one of said radiation elements.

9. The antenna system of claim 1 wherein the number N of radiation elements is sufficient to force substantially circularly symmetric propagation modes of electromagnetic energy.

10. The antenna system of claim 1 wherein the number N of radiation elements is eight.

11. The antenna system of claim 10 wherein said radiation elements comprise four pairs of opposed elements.

12. The antenna system of claim 9 wherein said network circuit means includes first, second, third and fourth 180°

hybrid networks, each having sum and difference ports and two side arm ports, and wherein the side arm ports of each hybrid network are coupled one each to one element of an element pair.

13. The antenna system of claim 1 further comprising sum signal means for providing antenna system sum signals characterized by substantial symmetry about the antenna boresight.

14. In a cylindrical cavity-backed antenna system having N radiation elements disposed adjacent the top surface of the cavity and spaced about a center axis of the cavity, and a feed system coupled to such elements, the improvement comprising:

N is at least six;

the radiation elements comprise substantially identical, substantially planar, non-interleaved elements of a polygon shape arranged in a closely packed, substantially symmetrical configuration about the axis of said cavity; and

network circuit means coupled to the feed means for producing an antenna system sum signal and an antenna system difference signal.

15. The improvement of claim 14 wherein said network circuit means coupled to said feed system has N signal ports for coupling one to each radiation element, said network circuit means including first and second phase shifting circuits, said first phase shifting circuit arranged to introduce progressive phase shifts of 360°

/N to signals associated with said respective elements to produce said sum signal, and said second phase shifting circuit arranged to introduce progressive phase shifts of 720°

/N to the signals associated with said respective elements to produce said difference signal.

16. The improvement of claim 15 wherein said number of elements N is eight, and wherein said first phase shifting network is adapted to introduce 45°

phase shifts, and said second phase shifting circuit is adapted to introduce 90°

phase shifts.

17. The improvement of claim 16 wherein said antenna system is adapted to communicate electromagnetic radiation of the right circular polarization (RCP) sense and left circular polarization (LCP) sense.

18. The improvement of claim 17 wherein said first phase shift circuit further comprises a first LCP port and a first RCP port, and said second phase shift circuit comprises a second LCP port and a second RCP port.

19. The improvement of claim 18 wherein said antenna system is utilized in an angle of arrival detection system comprising radar receiver means and radar resolver means.

20. The improvement of claim 19 wherein said receiver means comprises a four channel means and wherein said first and second LCP and RCP ports are respectively coupled to one of the channels of said receiver means.

27. The improvement of claim 14 wherein rhe radiation elements comprise substantially identical, substantially planar elements of a polygon shape arranged in a closely packed, substantially symmetrical configuration about the axis of said cavity.

21. An antenna system comprising:

first and second coaxially disposed conductive cylinders of a first diameter and a second diameter, each having first end regions, the first end regions of said cylinders being in substantial transverse alignment;

a first transverse conductive member disposed across and conductively joined across said first cylinder so as to define a first cavity inside said first conductive cylinder;

an annular second transverse conductive member disposed laterally between and conductively joined to said first and second conductive cylinders so as to define a second cavity in the annular region between said first and second cylinders;

a first set of N conductive radiation elements extending outwardly in a general radial direction from the center axis of said first cavity toward the adjacent first cylinder and generally equally spaced from adjacent elements, said radiation elements being insulated from said cylinders and being substantially parallel to the plane formed by said first end region of said first conductive cylinder, wherein N is at least six;

a second set of P conductive radiation elements extending outwardly in a general radial direction from adjacent the first cylinder toward the second cylinder, said radiation elements being insulated from said cylinders and being substantially parallel to the plane formed by said first end region of said second cylinder, wherein P is at least six;

difference signal means coupled to said first set of radiation elements and arranged to produce one difference signal characterized by a difference signal pattern which is substantially symmetrical in space about the angenna boresight; and

second difference signal means coupled to said second set of radiation elements and arranged to produce a second difference signal characterized by a difference signal pattern which is substantially symmetrical in space about the antenna boresight.

22. The antenna system of claim 21 wherein said first cylinder has a first diameter of at least 50% of a first wavelength of the lower band-edge frequency of a first antenna frequency band, and said second cylinder has a second diameter of at least 50% of a second wavelength of the lower band-edge frequency of a second antenna frequency band.

23. The antenna system of claim 22 wherein said first cavity has a depth approximately equal to 25% of the wavelength at the mid-band frequency of said first frequency band, and said second cavity has a depth of approximately 25% of the wavelength of the mid-band frequency of said second frequency band.

24. The antenna system of claim 23 wherein said first and second sets of radiation elements are disposed on a dielectric disc member disposed adjacent said first ends of said first and second cylinders.

25. The antenna system of claim 21 wherein said difference signal means and said sets of radiation elements are arranged to force circularly symmetric propagation modes of electromagnetic energy.

28. The improvement of claim 21 wherein the radiation elements comprise substantially identical, substantially planar elements of a polygon shape arranged in a closely packed, substantially symmetrical configuration about the axis of said cavity.

26. An antenna system comprising:

a plurality of coaxially disposed conductive cylinders of progressively larger diameters, each having first and second end regions, the first end regions of said cylinders being in substantial transverse alignment.

a plurality of transverse conductive members disposed across and conductively joined to said cylinders defining a cylindrical inner cavity and annular outer cavities.

a plurality of sets of conductive radiation elements disposed generally on concentric rings, the first set equally spaced about the center axis of the cylinders and extending generally radially outward above said inner cavity, and the succeeding rings respectively equally spaced and extending generally radially outwardly above the successive annular cavities each set having at least six radiation elements; and

a plurality of difference signal means coupled respectively to each set of radiation elements and arranged to produce a plurality of difference signals each characterized by a difference signal pattern having substantial symmetry about the antenna system boresight.