Electronically roll stabilized and reconfigurable active array system

Claim 2

An active array system for providing electronically roll stabilized array difference patterns, comprising: an array of spaced radiative elements forming a radiative aperture for receiving electromagnetic radiation; a plurality of active modules respectively coupled one each to each radiative element, each module comprising a first means for selectively phase shifting the radiation received at the corresponding radiative element by relative phase shifts of substantially 0 degrees or 180 degrees in dependence on a first module control signal to provide a first module receive signal; means for combining the respective first module receive signals to provide a first difference channel output signal; means for providing attitude position signals representing the relative attitude position of the array in relation to a reference position; and control means responsive to said attitude position signals for providing respective first module control signals to each of said plurality of modules for selectively controlling said first phase shifting means of each module to selectively and independently phase shift the radiation received at each radiative element so as to roll stabilize said first difference channel output signal in relation to said reference position.

Claim 3

The active array system of claim 1 wherein said control means adaptively partitions said aperture into roll-stabilized sectors and adaptively assigns each radiative element to a particular one of said sectors in dependence on said attitude position signals by controlling the state of said first phase shifting means.

Claim 4

The active array system of claim 1 wherein each of said modules further comprises a second phase shifting means for selectively phase shifting the radiation received at the corresponding radiative element by relative phase shifts of substantially 0 degrees or 180 degrees to provide a second module receive signal, said system further comprises means for combining the respective second module receive signals to provide a second difference channel output signal, and wherein said control means further comprises means responsive to said attitude position signals for providing respective second module control signals to each of said plurality of modules for selectively controlling said respective second phase shifting means of each module to selectively and independently phase shift the radiation received at each radiative element so as to roll stabilize said second difference channel output signal in relation to said reference position.

Claim 5

The active array system of claim 3 wherein said reference position is aligned with the azimuth, and said first difference channel output signal represents a roll-stabilized azimuth difference signal and said second difference channel output signal represents a roll-stabilized elevation difference signal.

Claim 6

The active array system of claim 4 wherein said control means partitions said array into roll-stabilized quadrant sectors and for each of the first and second difference channels adaptively assigns each radiative element to a particular quadrant by controlling the states of said first and second phase shifting means.

Claim 7

The active array system of claim 1 wherein said array of spaced radiative elements are disposed in a plane to provide a planar array.

Claim 8

An airborne active array system mounted in an aircraft or other airborne vehicle for providing electronically roll stabilized array difference patterns, comprising: a plurality of spaced radiative elements forming a radiative aperture for receiving electromagnetic radiation: means for providing attitude position signals representing the relative attitude position of the vehicle in relation to a reference position; a plurality of active modules respectively coupled one to each radiative element, each of said modules comprising an active amplifier for providing an amplified receive signal for the respective element, power dividing means for dividing the power of the amplified signal into first, second and third receive signal components, and first and second bi-state phase shifting means for respectively and selectively phase shifting the first and second amplified signal component by 0 degrees or 180 degrees in dependence of first and second bi-state control signals to provide first and second module difference signal components; first summing network for summing the respective first difference signal components from each module in the array to provide a first array difference signal; second summing network for summing the respective second difference signal components from each module in the array to provide a second array difference signal; and phase shifter control means for generating said first and second bi-state control signals and independently controlling said first and second phase shifters of each module in dependence on said attitude position signals to selectively and independently phase shift said first and second amplified signal components so as to roll stabilize the first and second difference patterns in relation to said reference position.

Claim 9

An airborne active array system mounted in an aircraft or other airborne vehicle for providing electronically roll stabilized array difference patterns, comprising: a plurality of spaced radiative elements forming a radiative aperture for receiving electromagnetic radiation: means for providing attitude position signals representing the relative attitude position of the vehicle in relation to a reference position; a plurality of active modules respectively coupled one to each radiative element, each of said modules comprising an active amplifier for providing an amplified receive signal for the respective element, power dividing means for dividing the power of the amplified signal into first, second and third receive signal components, and first and second bi-state phase shifting means for respectively and selectively phase shifting the first and second amplified signal component by 0 degrees or 180 degrees in dependence of first and second bi-state control signals to provide first and second module difference signal components; first summing network for summing the respective first difference signal components from each module in the array to provide a first array difference signal; second summing network for summing the respective second difference signal components from each module in the array to provide a second array difference signal; and phase shifter control means for generating said first and second bi-state control signals and independently controlling said first and second phase shifters of each module in dependence on said attitude position signals to selectively and independently phase shift said first and second amplified signal components so as to roll stabilize the first and second difference patterns in relation to said reference position.

Claim 10

The array system of claim 7 further comprising a third summing network for summing the respective third signal components from the respective power dividers to provide an array sum signal.

Claim 11

The array system of claim 7 wherein said radiative aperture is partitioned into roll-adapted quadrant sectors, and wherein said control means is adapted to set the first bi-state phase shifters of the modules associated with radiative elements in first and second adjacent quadrants to the 0 degree state, and those first bi-state phase shifters of the modules associated with radiative elements in the remaining adjacent third and fourth quadrants to the 180 degree state.

Claim 12

The array system of claim 9 wherein said control means is further adapted to set the second bi-state phase shifters of the modules associated with radiative elements in the adjacent first and fourth quadrants to the 0 degree state, and those second bi-state phase shifters of modules associated with radiative elements in the adjacent second and fourth quadrants to the 180 degree state.

Claim 13

The array system of claim 10 wherein said control means adaptively reconfigures the quadrant relationship of each radiative element in response to said attitude position signals by setting the bi-state phase shifters in the associated module to the appropriate state.

Claim 14

The active array system of claim 7 wherein said plurality of spaced radiative elements are disposed in a plane to provide a planar array.

Claim 15

An active array system usable in a multimode radar for simultaneously forming three independent electronically reconfigurable receive apertures from an active array radiative aperture, comprising a plurality of spaced radiative elements forming said radiative aperture for receiving electromagnetic radiation; a plurality of active modules respectively coupled one to a radiative element, each of said modules comprising an active amplifier for providing an amplified receive signal for the respective element, power dividing means for dividing the power of the amplified signal into first, second and third receive signal components, said first signal component providing a first module output signal, and first and second bi-state phase shifting means for selectively and independently shifting the second and third signal components by 0 degrees or 180 degrees in dependence on first and second control signals to provide second and third module output signals; first summing network coupled to said plurality of modules for summing the respective first module output signals to provide an array sum signal; second summing network coupled to said plurality of modules for summing the respective second module output signals to provide a first difference signal; third summing network coupled to said plurality of modules for summing the respective third module output signals to provide a second difference signal; and system processor for selecting an aperture configuration of said three apertures required by a particular mode in a multimode radar system, said processor adapted to provide said first and second control signals so as to selectively and independently shift the phase of said second and third signal components by 0° or 180°, said processor arranged to process said sum signals and said first and second difference signals to provide first, second, and third independent aperture signals.

Claim 16

An active array system usable in a multimode radar for simultaneously forming three independent electronically reconfigurable receive apertures from an active array radiative aperture, comprising a plurality of spaced radiative elements forming said radiative aperture for receiving electromagnetic radiation; a plurality of active modules respectively coupled one to a radiative element, each of said modules comprising an active amplifier for providing an amplified receive signal for the respective element, power dividing means for dividing the power of the amplified signal into first, second and third receive signal components, said first signal component providing a first module output signal, and first and second bi-state phase shifting means for selectively and independently shifting the second and third signal components by 0 degrees or 180 degrees in dependence on first and second control signals to provide second and third module output signals; first summing network coupled to said plurality of modules for summing the respective first module output signals to provide an array sum signal; second summing network coupled to said plurality of modules for summing the respective second module output signals to provide a first difference signal; third summing network coupled to said plurality of modules for summing the respective third module output signals to provide a second difference signal; and system processor for selecting an aperture configuration of said three apertures required by a particular mode in a multimode radar system, said processor adapted to provide said first and second control signals so as to selectively and independently shift the phase of said second and third signal components by 0° or 180°, said processor arranged to process said sum signals and said first and second difference signals to provide first, second, and third independent aperture signals.

Claim 17

The array system of claim 13 wherein said system processor comprises means for summing said first and second difference signals and dividing the sum by two to form a first aperture receive signal.

Claim 18

The array system of claim 13 wherein said system processor comprises means for substracting the second difference signal from the sum signal and dividing the difference by one-half to form a second aperture receive signal.

Claim 19

The array system of claim 13 wherein said system processor comprises means for substracting said second difference signal from said sum signal and dividing the difference signal by one-half to form a third aperture receive signal.

Claim 20

The array system of claim 13 further comprising means for providing attitude position signals representing the relative attitude position of said array in relation to a reference position, and wherein said system processor adaptively reconfigures the aperture relationship of each radiative element in response to said attitude position signals by setting the bi-state phase shifters in the associated module to the appropriate state in order to roll stabilize said three apertures.

Claim 21

The active array of claim 13 further comprising means for providing attitude position signals representing the relative attitude position of said array in relation to a reference position, said system processor being responsive to said attitude position signals to roll stabilize said respective apertures in relation to said reference position.

Claim 22

The active array system of claim 13 wherein said plurality of spaced radiative elements are disposed in a plane to provide a planar array.