PHASED ARRAY ANTENNA

• US 20190237869A1
• Filed: 06/07/2018
• Published: 08/01/2019
• Est. Priority Date: 06/09/2017
• Status: Active Grant

• Current Assignee: Mitsubishi Electric Corporation
• Original Assignee: Mitsubishi Electric Corporation
• Inventors: TAKAHASHI, Tomohiro
• Granted Patent: US 10,446,928 B2
• Time in Patent Office: Days
• CPC Class Codes: H01Q 1/28 Adaptation for use in or on aircraft, missiles, satellites, or balloons
• CPC Class Codes: H01Q 3/28 varying the amplitude
• CPC Class Codes: H01Q 3/30 varying the relative phase between the radiating elements of an array H01Q3/2605, H01Q3/2658, H01Q3/2682, H01Q3/44 take precedence
• CPC Class Codes: H04B 7/06 at the transmitting station

Abstract

A phased array antenna includes a signal source, a distribution circuit, phase shifters, amplifiers, antenna elements, and a control device. The signal source generates a signal. The distribution circuit divides the signal generated by the signal source. The phase shifters shift phases of signals divided by the distribution circuit to change an orientation direction in which electromagnetic wave is emitted. The amplifiers amplify signals output by the phase shifters. The antenna elements emit, as the electromagnetic wave, signals output by the amplifiers. The control device controls the amplifiers such that, in a plane that is parallel to an orbital plane of a satellite with which communication of the electromagnetic wave is established, amplitudes of amplifiers, among the amplifiers, which are arranged in the center of the plane are greater than amplitudes of amplifiers, among the amplifiers, arranged at the periphery.

Claims

1-8. -8. (canceled)

9. :

A phased array antenna comprising;

a signal source to generate a signal;

a distribution circuit to divide the signal generated by the signal source;

phase shifters to shift phases of signals divided by the distribution circuit;

amplifiers to amplify signals output by the phase shifters;

antenna elements arranged on a plane to emit, as an electromagnetic wave, the signals output by the amplifiers; and

a control device to control the amplifiers such that, in an intersection line between a plane that is parallel to an orbital plane of a satellite with which communication of the electromagnetic wave is established and the plane on which the antenna elements are arranged, amplitudes of amplifiers, among the amplifiers, that are connected to antenna elements, among the antenna elements, arranged in a center of the plane are greater than amplitudes of amplifiers, among the amplifiers, that are connected to antenna elements, among the antenna elements, arranged at a periphery of the plane.

10. :

The phased array antenna according to claim 9, wherein

the control device controls the amplifiers such that, in a plane parallel to the orbital plane, amplitudes of amplifiers, among the amplifiers, which are arranged in a center of the plane are greater than amplitudes of the amplifiers arranged at the periphery of the plane so that the electromagnetic wave has a low side lobe characteristic on the orbital plane.

11. :

The phased array antenna according to claim 9, wherein

the control device controls the amplifiers to form a uniform amplitude in a plane of the electromagnetic wave that is perpendicular to the orbital plane.

12. :

The phased array antenna according to claim 10, wherein

the control device controls the amplifiers to form a uniform amplitude in a plane of the electromagnetic wave that is perpendicular to the orbital plane.

13. :

The phased array antenna according to claim 9, wherein

the control device comprises;

a moving body information acquirer to acquire information about a moving body on which the antenna elements are disposed;

a satellite information acquirer to acquire information about the satellite;

an orientation direction calculator to calculate, from the information about the moving body and the information about the satellite, an orientation direction of the electromagnetic wave emitted;

a location calculator to calculate a relative position between the orbital plane and the moving body and then calculate, from the calculated relative position, an angle of the plane of the electromagnetic wave parallel to the orbital plane;

a phase shift value calculator to calculate a phase shift value relative to each of the phase shifters for directing the electromagnetic wave in the orientation direction; and

an amplification value calculator to calculate, from the angle of the plane parallel to the orbital plane, an amplification value relative to each of the amplifiers.

14. :

The phased array antenna according to claim 10, wherein

the control device comprises;

a moving body information acquirer to acquire information about a moving body on which the antenna elements are disposed;

a satellite information acquirer to acquire information about the satellite;

an orientation direction calculator to calculate, from the information about the moving body and the information about the satellite, an orientation direction of the electromagnetic wave emitted;

a location calculator to calculate a relative position between the orbital plane and the moving body and then calculate, from the calculated relative position, an angle of the plane of the electromagnetic wave parallel to the orbital plane;

a phase shift value calculator to calculate a phase shift value relative to each of the phase shifters for directing the electromagnetic wave in the orientation direction; and

an amplification value calculator to calculate, from the angle of the plane parallel to the orbital plane, an amplification value relative to each of the amplifiers.

15. :

The phased array antenna according to claim 11, wherein

the control device comprises;

a moving body information acquirer to acquire information about a moving body on which the antenna elements are disposed;

a satellite information acquirer to acquire information about the satellite;

an orientation direction calculator to calculate, from the information about the moving body and the information about the satellite, an orientation direction of the electromagnetic wave emitted;

a location calculator to calculate a relative position between the orbital plane and the moving body and then calculate, from the calculated relative position, an angle of the plane of the electromagnetic wave parallel to the orbital plane;

a phase shift value calculator to calculate a phase shift value relative to each of the phase shifters for directing the electromagnetic wave in the orientation direction; and

an amplification value calculator to calculate, from the angle of the plane parallel to the orbital plane, an amplification value relative to each of the amplifiers.

16. :

The phased array antenna according to claim 9, wherein

the control device stops functioning of a part of the phase shifters and a part of the amplifiers to reduce an antenna aperture size.

17. :

The phased array antenna according to claim 10, wherein

the control device stops functioning of a part of the phase shifters and a part of the amplifiers to reduce an antenna aperture size.

18. :

The phased array antenna according to claim 11, wherein

the control device stops functioning of a part of the phase shifters and a part of the amplifiers to reduce an antenna aperture size.

19. :

The phased array antenna according to claim 12, wherein

the control device stops functioning of a part of the phase shifters and a part of the amplifiers to reduce an antenna aperture size.

20. :

The phased array antenna according to claim 13, wherein

the control device further comprises;

a gain calculator to calculate a gain relative to the orientation direction calculated by the orientation direction calculator, calculate, form the information about the moving body and the information about the satellite, a gain necessary for communication between the moving body and the satellite, and calculate a difference between the calculated gain necessary for the communication and the gain relative to the orientation direction; and

an antenna aperture size controller to calculate an antenna aperture size corresponding to the difference and then stop functioning of amplifiers, among the amplifiers, and phase shifters, among the phase shifters, that correspond to the antenna aperture size corresponding to the calculated difference.

21. :

The phased array antenna according to claim 14, wherein

the control device further comprises;

a gain calculator to calculate a gain relative to the orientation direction calculated by the orientation direction calculator, calculate, form the information about the moving body and the information about the satellite, a gain necessary for communication between the moving body and the satellite, and calculate a difference between the calculated gain necessary for the communication and the gain relative to the orientation direction; and

an antenna aperture size controller to calculate an antenna aperture size corresponding to the difference and then stop functioning of amplifiers, among the amplifiers, and phase shifters, among the phase shifters, that correspond to the antenna aperture size corresponding to the calculated difference.

22. :

The phased array antenna according to claim 15, wherein

the control device further comprises;

a gain calculator to calculate a gain relative to the orientation direction calculated by the orientation direction calculator, calculate, form the information about the moving body and the information about the satellite, a gain necessary for communication between the moving body and the satellite, and calculate a difference between the calculated gain necessary for the communication and the gain relative to the orientation direction; and

an antenna aperture size controller to calculate an antenna aperture size corresponding to the difference and then stop functioning of amplifiers, among the amplifiers, and phase shifters, among the phase shifters, that correspond to the antenna aperture size corresponding to the calculated difference.

23. :

The phased array antenna according to claim 20, wherein

the antenna aperture size controller causes amplifiers, among the amplifiers, and phase shifters, among the phase shifters, that are arranged in a rectangular shape to operate without stopping the amplifiers arranged in the rectangular shape and the phase shifters arranged in the rectangular shape, and

one of diagonals of the rectangular shape is included in the plane parallel to the orbital plane.

24. :

The phased array antenna according to claim 21, wherein

the antenna aperture size controller causes amplifiers, among the amplifiers, and phase shifters, among the phase shifters, that are arranged in a rectangular shape to operate without stopping the amplifiers arranged in the rectangular shape and the phase shifters arranged in the rectangular shape, and

one of diagonals of the rectangular shape is included in the plane parallel to the orbital plane.

25. :

The phased array antenna according to claim 22, wherein

the antenna aperture size controller causes amplifiers, among the amplifiers, and phase shifters, among the phase shifters, that are arranged in a rectangular shape to operate without stopping the amplifiers arranged in the rectangular shape and the phase shifters arranged in the rectangular shape, and

one of diagonals of the rectangular shape is included in the plane parallel to the orbital plane.

26. :

The phased array antenna according to claim 13, wherein

the moving body is an aircraft.

27. :

The phased array antenna according to claim 20, wherein

the moving body is an aircraft.

28. :

The phased array antenna according to claim 23, wherein

the moving body is an aircraft.