Low profile antenna for satellite communication

• US 20060197713A1
• Filed: 02/18/2004
• Published: 09/07/2006
• Est. Priority Date: 02/18/2003
• Status: Active Grant

• Current Assignee: Panasonic Avionics Corporation (Panasonic Holdings Corporation)
• Original Assignee: Starling Advanced Communications Ltd.
• Inventors: Berdnikova, Valentina, Mansour, David, Erlich, Simha
• Granted Patent: US 7,629,935 B2
• Time in Patent Office: Days
• US Class Current: 343/882
• CPC Class Codes: H01Q 21/061 Two dimensional planar arrays
• CPC Class Codes: H01Q 21/29 Combinations of different interacting antenna units for giving a desired directional characteristic H01Q25/00 takes precedence
• CPC Class Codes: H01Q 3/04 for varying one co-ordinate of the orientation
• CPC Class Codes: H01Q 3/08 for varying two co-ordinates of the orientation

Abstract

A low profile receiving and/or transmitting antenna includes an array of antenna elements that collect and coherently combine millimeter wave or other radiation. The antenna elements are physically configured so that radiation at a predetermined wavelength band impinging on the antenna at a particular angle of incidence is collected by the elements and collected in-phase. Two or more mechanical rotators may be disposed to alter the angle of incidence of incoming or outgoing radiation to match the particular angel of incidence.

Claims

1. An antenna comprising:

a support frame;

a plurality of antenna panels movably coupled to the support frame and having a variable beam direction relative to the support frame; and

at least one actuator adapted to change the beam direction of the plurality of antenna panels, so as to track a transmitter or receiver, such that each pair of adjacent antenna panels substantially border each other as projected onto a plane perpendicular to the beam direction, and wherein when viewed from a predetermined range of the beam direction, none of the antenna panels is covered partially or totally by any other panel.

3. The antenna of claim 1, wherein the antennal panels are rotatably connected to said support frame on respectively associated parallel axes of rotation and are parallely movable with respect to each other along lines which are perpendicular to said axes of rotation.

7. The antenna of claim 1, wherein the at least one actuator is adapted to change the beam direction while maintaining the antenna gain substantially the same as for a single antenna with an aperture similar to the sum of all the then active antenna panel apertures.

8. The antenna of claim 1, wherein the support frame is rotatable under control of the at least one actuator.

9. The antenna of claim 1, wherein the at least one actuator comprises a pneumatic actuator.

10. The antenna of claim 1, wherein the at least one actuator comprises an electrical actuator.

11. The antenna of claim 1, wherein the at least one actuator comprises a linear actuator.

12. The antenna of claim 1, wherein the at least one actuator comprises a motor.

13. The antenna of claim 1, wherein a plurality of antenna elements are disposed on each antenna panel.

14. The antenna of claim 1, wherein Abeam directions of the antenna panels are aligned along a common beam focus direction.

15. The antenna of claim 1, wherein the plurality of antenna panels comprise at least four antenna panels.

2. (canceled)

4-5. -5. (canceled)

6. The antenna of claim 43, further comprising at least one auxiliary panel which can be made active and which is rotatable about an axis parallel to the rotational axes of said antenna panels only for a limited range relative to the elevation angle of rotation of said antenna panels.

16. A method for receiving or transmitting electrical signals by an antenna, said method comprising:

providing a plurality of antenna panels having variable beam directions;

directing the beam directions of the antenna panels toward a transmitter or receiver; and

changing the beam directions of the antenna panels to define a common beam direction, so as to track the transmitter or receiver, the common beam direction being changed such that each pair of adjacent antenna panels substantially border each other as projected onto a plane perpendicular to the common beam direction, and wherein, when viewed from a predetermined range of the common beam direction, none of the antenna panels is covered partially or totally by any other panel.

17. The method of claim 16, wherein said active antenna panels are directed by at least one actuator.

18. The method of claim 16, wherein said antenna panels are parallel to each other and rotated in elevation and azimuth and variably spaced apart from one another using at least one actuator.

19. The method of claim 16, further comprising mounting the antenna panels on an aircraft in a common support structure.

20. An RF antenna array comprising:

a plurality of panels, each panel carrying a sub-array of RF antenna elements defining an RF radiation pattern having a principal beam direction;

at least one elevational angle driving mechanism;

at least one azimuthal angle driving mechanism;

at least one linear translation driving mechanism;

each said panel being mounted for angular movement by an elevational angle driving mechanism about a respective one of parallel first axes so as to steer elevational angles of corresponding sub-array pattern beams along substantially parallel lines;

each said panel also being mounted for movement by an azimuthal angle driving mechanism about a common second axis, substantially perpendicular to said first axes, so as to steer azimuthal angles of corresponding sub-array pattern beams; and

at least one of said panels also being mounted for translational movement with respect to at least one other of said panels by a linear translation driving mechanism along a linear axis that is substantially perpendicular to said first axes and to said second axis.

21. An RF antenna array as in claim 20 wherein said driving mechanisms are controlled so as to avoid substantial gaps between projections of said panels along their beam directions over a predetermined range of beam directions.

22. An RF antenna array as in claim 20 wherein said driving mechanisms are controlled so as to avoid substantial overlaps between projections of said panels along their beam directions over a predetermined range of beam directions.

23. An RF antenna array as in claim 20 wherein said driving mechanisms are controlled so as to avoid substantial gaps between projections of said panels along their beam directions over a predetermined range of beam directions and so as to avoid substantial overlaps between projections of said panels along their beam directions over a predetermined range of beam directions.

24. A method of operating an RF antenna array, said method comprising:

disposing a sub-array of RF antenna elements defining an RF radiation pattern having a principal beam direction over each of plural individually controllable panels;

angularly moving each said panel about a respective one of parallel first axes so as to steer elevational angles of corresponding sub-array pattern beams along substantially parallel lines;

angularly moving each said panel about a common second axis, substantially perpendicular to said first axes, so as to steer azimuthal angles of corresponding sub-array pattern beams; and

translationally moving at least one of said panels with respect to at least one other of said panels along a linear axis that is substantially perpendicular to said first axes and to said second axis.

25. A method as in claim 24 further comprising moving said panels about and along said axes so as to avoid substantial gaps between projections of said panels along their beam directions over a predetermined range of beam directions.

26. A method as in claim 24 further comprising moving said panels about and along said axes so as to avoid substantial overlaps between projections of said panels along their beam directions over a predetermined range of beam directions.

27. A method as in claim 24 further comprising moving said panels about and along said axes so as to avoid substantial gaps between projections of said panels along their beam directions over a predetermined range of beam directions and so as to avoid substantial overlaps between projections of said panels along their beam directions over a predetermined range of beam directions.

28. An RF antenna array comprising:

a plurality of panels, each panel carrying a sub-array of RF antenna elements defining an RF radiation pattern having a principal beam direction;

each panel being mounted for coordinated movements in elevational angle, azimuthal angle and separation distance therebetween so as to track an RF target in elevation and azimuth while maintaining mutually parallel principal beam directions for said sub-arrays such that projections of adjacent sub-arrays taken along their respective parallel principal beam directions are approximately contiguous, without substantial gap or substantial overlap, over a range of elevational angles.

29. An RF antenna array as in claim 28 further comprising:

at least three movement actuators coupled to said panels for independent control of said movements in elevational angle, azimuthal angle and separation distance respectively.

30. An RF antenna array as in claim 28 wherein the inter-panel separation distance D between corresponding points of adjacent panels having width d_L and elevational angle α

is substantially D=d_L/sin(α

) over said range of elevational angles.

31. An RF antenna array as in claim 28 wherein said panels are mounted for linear translational movement along a common linear axis to adjust the inter-panel separation distance.

32. A method of operating an RF antenna array, said method comprising:

disposing a sub-array of RF antenna elements defining an RF radiation pattern having a principal beam direction on each of plural panels;

controlling coordinated movements of each panel in elevational angle, azimuthal angle and separation distance therebetween so as to track an RF target in elevation and azimuth while maintaining mutually parallel principal beam directions for said sub-array such that projections of adjacent sub-arrays taken along their respective parallel principal beam directions are approximately contiguous, without substantial gap or substantial overlap, over a range of elevational angles.

33. A method as in claim 32 further comprising:

controlling at least three movement actuators coupled to said panels for independent control of said movements in elevational angle, azimuthal angle and separation distance respectively.

34. A method as in claim 32 wherein the inter-panel separation distance D between corresponding points of adjacent panels having width d_L and elevational angle α

is substantially D=d_L/sin(α

) over said range of elevational angles.

35. A method as in claim 32 wherein said panels are linearly translated along a common linear axis to adjust the inter-panel separation distance.