Dielectric-resonator array antenna system

• US 20050264449A1
• Filed: 06/01/2004
• Published: 12/01/2005
• Est. Priority Date: 06/01/2004
• Status: Active Grant

• Current Assignee: EMS Technologies Canada Ltd. (Honeywell International Inc.)
• Original Assignee: EMS Technologies Canada Ltd. (Honeywell International Inc.)
• Inventors: Strickland, Peter C.
• Granted Patent: US 7,071,879 B2
• Time in Patent Office: Days
• US Class Current: 343/700.MS
• CPC Class Codes: H01Q 1/288 Satellite antennas
• CPC Class Codes: H01Q 21/064 using horn or slot aerials slotted waveguides arrays H01Q21/005
• CPC Class Codes: H01Q 9/0485 Dielectric resonator antennas

Abstract

A dielectric resonator element array (DRA) antenna system that is small, compact, has high gain in the direction of intended communication, minimized interference in unintended directions of communication and a wide bandwidth. The antenna system comprises a ground plane, a feed structure, a beam shaping and steering controller, a mounting apparatus, an array of dielectric resonator elements and a radome that is close to or in contact with the array. The mounting apparatus preferably is configured so as not to appreciably increase the size of the system when mounted. The controller receives and processes information relating to one or more of object latitude, longitude, attitude, direction of travel, intended direction of communication and unintended directions of communication. The controller processes this information and determines excitation phase for the array elements.

Claims

1. A dielectric resonator antenna system comprising:

a ground plain;

a feed structure;

an array of dielectric resonator elements electrically coupled to the feed structure, each dielectric element having a relatively high permittivity;

a radome close to or in contact with the array of dielectric resonator elements;

an object mounting apparatus for mounting the antenna system on an object; and

a beam shaping and steering controller, the beam shaping and steering controller controlling the feed structure to thereby control excitation phases of the dielectric resonator elements.

2. The dielectric resonator antenna system of claim 1, wherein the permittivity of the array elements is higher than that of free space, the elements having low conductivity and low loss tangent.

3. The dielectric resonator antenna system of claim 1, wherein the array elements are substantially rectangular parallelepiped in shape.

4. The dielectric resonator antenna system of claim 1, wherein the array elements are arranged on a nominally planar surface.

5. The dielectric resonator antenna system of claim 1, wherein the array elements are arranged in a nominally triangular grid.

6. The dielectric resonator antenna system of claim 1, wherein the elements are configured dimensionally such that the antenna system performs optimally with the resonators close to or in contact with the array.

7. The dielectric resonator antenna system of claim 1, wherein the controller sets the excitation phases of the elements such that interference in specific directions or regions is minimized.

8. The dielectric resonator antenna system of claim 1, wherein the controller receives information relating to an object on which the antenna system is mounted and uses the information to set excitation phases of the array elements, the information including one or more of object latitude, longitude, attitude, direction of travel, intended direction of communication and unintended directions of communication.

9. The dielectric resonator antenna system of claim 8, wherein the intended direction of communication is in a direction of a satellite with which communication is desired.

10. The dielectric resonator antenna system of claim 8, wherein the unintended directions are in directions of satellites with which communication is undesired.

11. The dielectric resonator antenna system of claim 8, wherein the antenna system is mounted on a mobile platform.

12. The dielectric resonator antenna system of claim 8, wherein the antenna system is mounted on a mobile platform selected from the group comprising an aircraft, a ship, a train, an automobile and a recreational vehicle (RV).

13. The dielectric resonator antenna system of claim 11, wherein the controller receives navigational and/or attitude input from navigational and/or attitude aids on the aircraft and uses the received information to set the excitation phases of the array elements.

14. The dielectric resonator antenna system of claim 1, wherein the controller receives information from one or more of an accelerometer, an Inertial Navigation System (INS), an Inertial Reference System (IRS), a global positioning system (GPS) receiver, and an inclinometer.

15. The dielectric resonator antenna system of claim 1, wherein the mounting apparatus comprising a sliding jam-clamp having a first portion and a second portion, the first portion being attached to the antenna system and the second portion being attached to the object, the first and second portions being configured to slidably engage each other in a friction-fit mating configuration, and wherein the mounting apparatus does not appreciably increase the size of the antenna system.

16. The dielectric resonator antenna system of claim 1, further comprising:

mounting hardware that passes through an opening or indentation in the radome and attaches to the array, and wherein the hardware, when attached, does not extend significantly beyond base portions of the array elements and consequently does not interfere with radiation characteristics of the antenna system.

17. The dielectric resonator antenna system of claim 1, wherein the controller executes a beam steering algorithm that takes into account information including one or more of object latitude, longitude, attitude, direction of travel, intended direction of communication and unintended directions of communication.

18. The dielectric resonator antenna system of claim 1, wherein the controller receives the information in real-time and sets the excitation phases in real-time as the information is processed in accordance with the beam steering algorithm being executed by the controller.

19. The dielectric resonator antenna system of claim 1, wherein the array elements each comprise a plastic base filled with a ceramic powder.

20. The dielectric resonator antenna system of claim 1, wherein the array elements are attached to a substrate of the feed structure by a Cyanoacrylate adhesive.

21. The dielectric resonator antenna system of claim 18, wherein the algorithm controls the beam shape such that a best possible trade-off between gain in the intended direction of communication and interference in the directions of unintended communication is achieved.

22. A method of communicating with a dielectric resonator array antenna, the method comprising:

receiving information in real-time in a beam shaping and steering controller, the information including one or more of object latitude, longitude, attitude, direction of travel, intended direction of communication and unintended directions of communication; and

processing the information in real-time in the controller in accordance with a beam shaping and steering control algorithm being executed by the controller to determine excitation phases for the array elements; and

exciting phases of the array elements in real-time based on the determinations made by the controller.

23. The method of claim 22, wherein the permittivity of the array elements is higher than that of free space, the elements having low conductivity and low loss tangent.

24. The method of claim 22, wherein the array elements are substantially rectangular parallelepiped in shape.

25. The method of claim 22, wherein the array elements are arranged on a nominally planar surface.

26. The method of claim 22, wherein the array elements are arranged in a nominally triangular grid.

27. The method of claim 22, wherein the excitation phases of the elements are set such that interference in specific directions or regions is minimized.

28. The method of claim 22, wherein the intended direction of communication is in a direction of a satellite with which communication is desired.

29. The method of claim 22, wherein the unintended directions are in directions of satellites with which communication is undesired.

30. The method of claim 22, wherein the antenna system is designed to communicate with satellites.

31. The method of claim 30, wherein the antenna system is mounted on a mobile platform.

32. The method of claim 22, wherein the antenna system is mounted on a mobile platform selected from the group comprising an aircraft, a ship, a train, an automobile and a recreational vehicle (RV).

33. The method of claim 22, wherein the information is received from one or more of an accelerometer, an Inertial Navigation System (INS), an Inertial Reference System (IRS), a global positioning system (GPS) receiver and an inclinometer.