Low cost space-fed reconfigurable phased array for spacecraft and aircraft applications

Patent metadata

Field	Value
Publication number	US-2016248157-A1
Application number	US-201514627053-A
Country	US
Kind code	A1
Filing date	Feb 20, 2015
Priority date	Feb 20, 2015
Publication date	Aug 25, 2016
Grant date	—

Abstract

A phased array antenna system including a front-end circuit having a plurality of antenna channels, each including a front antenna element and a rear antenna element, that provides a spatially combined beam. Each antenna channel includes a beam scan phase shifter and a true time delay phase shifter through which the receive signals or the transmit signals propagate. The system further includes a back-end circuit spaced from the front-end circuit and including an antenna receiving the receive signals from the rear elements or transmitting the transmit signals to the rear elements. The back-end circuit further includes an ortho-mode transducer that separates the transmit signal or the receive signal into orthogonally polarized signals, and a pair of couplers and a pair of polarization phase shifters that combine to adjust the polarization of the transmit signal or the receive signal. The spatially combined beam is reconfigurable in beam shape and its location.

First claim

What is claimed is:

1 . A phased array antenna system comprising:
a front-end circuit including a plurality of antenna channels where each antenna channel includes a front antenna element and a rear antenna element, said front antenna element being operable to receive signals from the environment or transmit signals into the environment, each antenna channel further including a beam scan phase shifter and a true time delay (TTD) phase shifter through which the receive signals or the transmit signals propagate; and a back-end circuit spaced apart from the front-end circuit and including an antenna receiving the receive signals from the rear antenna elements or transmitting the transmit signals to the rear antenna elements, said back-end circuit further including an ortho-mode transducer that separates the transmit signal or the receive signal into orthogonally polarized signals, said back-end circuit further including a pair of couplers and a pair of polarization phase shifters that combine to adjust the polarization of the transmit signal or the receive signal.

2 . The antenna system according to claim 1 wherein each antenna channel includes a variable attenuator positioned between the beam scan phase shifter and the TTD phase shifter that provides signal attenuation.

3 . The antenna system according to claim 1 wherein each antenna channel includes an amplifier positioned between the beam scan phase shifter and the front antenna element that is a low noise amplifier for the receive signals from the environment or a high power amplifier for transmitting signals into the environment.

4 . The antenna system according to claim 1 wherein the pair of couplers include a first coupler and a second coupler, and wherein the ortho-mode transducer includes a first output coupled to a first input of the first coupler and a second output coupled to a second input of the first coupler, and wherein a first output of the first coupler is coupled to a first input of the second coupler and a second output of the first coupler is coupled to a second input of the second coupler.

5 . The antenna system according to claim 4 wherein the pair of phase shifters include a first phase shifter provided between the first output of the first coupler and the first input of the second coupler and a second phase shifter provided between the second output of the first coupler and the second input of the second coupler.

6 . The antenna system according to claim 4 wherein the pair of phase shifters include a first phase shifter provided between the second output of the ortho-mode transducer and the second input of the first coupler and a second phase shifter provided between the second output of the first coupler and the second input of the second coupler.

7 . The antenna system according to claim 1 wherein the antenna system is configured to be provided on a spacecraft or an aircraft.

8 . The antenna system according to claim 1 wherein the front antenna elements and the rear antenna elements are selected from the group consisting of antenna horns, ring-slot elements, stacked patch elements, flared notch elements, ridged waveguide elements and bow-tie elements.

9 . The antenna system according to claim 1 wherein the beam scan phase shifters and the polarization phase shifters are modular 2π phase shifters.

10 . The antenna system according to claim 1 wherein the antenna in the back-end circuit is a feed horn.

11 . A phased array antenna system for a space-borne platform, said system comprising:
a front-end circuit including a plurality of antenna channels where each antenna channel includes a front antenna element and a rear antenna element, said front antenna element being operable to receive signals from the environment or transmit signals into the environment, each antenna channel further including a beam scan phase shifter and a true time delay (TTD) phase shifter through which the receive signals or the transmit signals propagate; and a back-end circuit spaced apart from the front-end circuit and including a fed horn receiving the receive signals from the rear antenna elements or transmitting the transmit signals to the rear antenna elements, said back-end circuit further including an ortho-mode transducer that separates the transmit signal or the receive signal into orthogonally polarized signals, and a first coupler and a second coupler, wherein the ortho-mode transducer includes a first output coupled to a first input of the first coupler and a second output coupled to a second input of the first coupler, and wherein a first output of the first coupler is coupled to a first input of the second coupler and a second output of the first coupler is coupled to a second input of the second coupler, said back-end circuit further including a first polarization phase shifter provided between the first output of the first coupler and the first input of the second coupler and a second polarization phase shifter provided between the second output of the first coupler and the second input of the second coupler, where the signals are reconfigurable in beam shape and location.

12 . The antenna system according to claim 11 wherein each antenna channel includes a variable attenuator positioned between the beam scan phase shifter and the TTD phase shifter that provides signal attenuation.

13 . The antenna system according to claim 11 wherein each antenna channel includes an amplifier positioned between the beam scan phase shifter and the front antenna element that is a low noise amplifier for the receive signals from the environment or a high power amplifier for transmitting signals into the environment.

14 . The antenna system according to claim 11 wherein the front antenna elements and the rear antenna elements are selected from the group consisting of antenna horns, ring-slot elements, stacked patch elements, flared notch elements, ridged waveguide elements and bow-tie elements.

15 . The antenna system according to claim 11 wherein the beam scan phase shifters and the polarization phase shifters are modular 2π phase shifters.

16 . A phased array antenna system for a space-borne platform, said system comprising:
a front-end circuit including a plurality of antenna channels where each antenna channel includes a front antenna element and a rear antenna element, said front antenna element being operable to receive signals from the environment or transmit signals into the environment, each antenna channel further including a beam scan phase shifter and a true time delay (TTD) phase shifter through which the receive signals or the transmit signals propagate; and a back-end circuit spaced apart from the front-end circuit and including a fed horn receiving the receive signals from the rear antenna elements or transmitting the transmit signals to the rear antenna elements, said back-end circuit further including an ortho-mode transducer that separates the transmit signal or the receive signal into orthogonally polarized signals, and a first coupler and a second coupler, wherein the ortho-mode transducer includes a first output coupled to a first input of the first coupler and a second output coupled to a second input of the first coupler, and wherein a first output of the first coupler is coupled to a first input of the second coupler and a second output of the first coupler is coupled to a second input of the second coupler, said back-end circuit further including a first polarization phase shifter provided between the second output of the ortho-mode transducer and the second input of the first coupler and a second polari

Assignees

• Northrop Grumman Systems Corp

Inventors

• Rao Sudhakar K
• Bhattacharyya Arun K

Classifications

• H01Q21/0018

  Space- fed arrays · CPC title

• H01Q13/0258

  Orthomode horns (orthomode transducers H01P1/161) · CPC title

• H01Q1/28

  Adaptation for use in or on aircraft, missiles, satellites, or balloons · CPC title

• H01Q3/2694 Primary

  using also variable phase-shifters (H01Q3/2688 takes precedence) · CPC title