Search-radar azimuth correction

Claim 2

In a radar system having a radar antenna mounted on a non-stable platform and a radar polar coordinate plan position indicator display, said radar antenna mounted on a non-stable platform being mounted on a craft or vehicle that is subject to motion and that has a stable reference source that is stable in attitude, the improvement comprising a correction system for generating a correction-to-azimuth signal, Cα, said correction system comprising: a computer having a first input connected to said stable reference source, having a second input connected to said radar antenna, and having at least a first output; means having a first input connected to said antenna and a second input connected to said first computer output for generating an output signal that comprises said correction-to-azimuth signal, Cα, said means having an output that is connected to said radar display; and further wherein: said radar antenna is not mounted on a platform that moves independently with respect to the motion of said craft or vehicle and wherein said non-stable platform does not move independently with respect to the motion of said craft or vehicle; and wherein said correction-to-azimuth signal, C.sub.α, is the correction angle which must be added to the antenna radar azimuth angle, α, to obtain the true value of the azimuth of the target in the horizontal plane relative to the projection of the longitudinal axis of said craft or vehicle in the horizontal plane.

Claim 3

The system of claim 1 wherein: said stable reference source provides a first output that is proportional to the deviation in pitch, θ, of said craft from a reference pitch position, and a second output that is proportional to the deviation in roll, φ, of said craft from a reference roll position; said computer being connected to receive said first and second outputs of said stable reference source.

Claim 4

The system of claim 2 wherein said computer receives a target azimuth signal, α, from said radar antenna.

Claim 5

The system of claim 3 wherein: said means for generating an output signal comprises a solid state control differential transmitter.

Claim 6

The system of claim 4 wherein said output signal of said solid state control differential transmitter comprises the sum of C.sub.α and α.

Claim 7

The system of claim 3 wherein said means for generating an output signal that is comprised of the sum of C.sub.α and α.

Claim 8

In a radar system having a radar antenna mounted on a non-stable platform and a radar polar coordinate display, said radar antenna mounted on a non-stable platform being mounted on a craft or vehicle that is subject to motion and that has a stable reference source that is stable in attitude, the improvement comprising a correction system for generating a correction-to-azimuth signal, C.sub.α, said correction system comprising: a computer having a first input connected to said stable reference source, having a second input connected to said radar antenna and having at least a first output; means having a first input connected to said antenna and a second input connected to said first computer output for generating an output signal that comprises said correction-to-azimuth signal, C.sub.α, said means having an output that is connected to said radar display; and further wherein: said radar antenna is not mounted on a platform that moves independently with resepct to the motion of said craft or vehicle and wherein said non-stable platform does not move independently with respect to the motion of said craft or vehicle, and wherein C 60 corresponds to the correction angle which must be added to the antenna radar azimuth angle to a target, α, to obtain the true value of the azimuth of the target in the horizontal plane relative to the projection of the ship's fore and aft longitudinal axis in the horizontal plane; and wherein said stable reference source provides a first output that is proportional to the deviation in pitch, θ, of said craft from a reference position, and a second output that is proportional to the deviation in roll, φ, of said craft from a reference roll position; said computer being connected to receive said first and second outputs of said stable reference source and receives a target azimuth signal corresponding to α from said radar antenna mounted on a non-stable platform; and where: C.sub.α =A-α; and where ##EQU6## where -45°≦α≦45° from a predetermined reference position; ##EQU7## where 135°≦α≦225° from said predetermined reference position; ##EQU8## where 45°<α<135° from said predetermined reference position; and ##EQU9## where 225°<α<315° from said predetermined reference position; where a 11 =cos θ a 12 =sin θ sin φ a 13 =sin θ cos φ a 21 =0 a 22 =cos φ a 23 =-sin φ a 31 =-sin θ a 32 =cos θ sin φ a 33 =cos θ cos φ

Claim 9

In a radar system having a radar antenna mounted on a non-stable platform and a radar polar coordinate display, said radar antenna mounted on a non-stable platform being mounted on a craft or vehicle that is subject to motion and that has a stable reference source that is stable in attitude, the improvement comprising a correction system for generating a correction-to-azimuth signal, C.sub.α, said correction system comprising: a computer having a first input connected to said stable reference source, having a second input connected to said radar antenna and having at least a first output; means having a first input connected to said antenna and a second input connected to said first computer output for generating an output signal that comprises said correction-to-azimuth signal, C.sub.α, said means having an output that is connected to said radar display; and further wherein: said radar antenna is not mounted on a platform that moves independently with resepct to the motion of said craft or vehicle and wherein said non-stable platform does not move independently with respect to the motion of said craft or vehicle, and wherein C 60 corresponds to the correction angle which must be added to the antenna radar azimuth angle to a target, α, to obtain the true value of the azimuth of the target in the horizontal plane relative to the projection of the ship's fore and aft longitudinal axis in the horizontal plane; and wherein said stable reference source provides a first output that is proportional to the deviation in pitch, θ, of said craft from a reference position, and a second output that is proportional to the deviation in roll, φ, of said craft from a reference roll position; said computer being connected to receive said first and second outputs of said stable reference source and receives a target azimuth signal corresponding to α from said radar antenna mounted on a non-stable platform; and where: C.sub.α =A-α; and where ##EQU6## where -45°≦α≦45° from a predetermined reference position; ##EQU7## where 135°≦α≦225° from said predetermined reference position; ##EQU8## where 45°<α<135° from said predetermined reference position; and ##EQU9## where 225°<α<315° from said predetermined reference position; where a 11 =cos θ a 12 =sin θ sin φ a 13 =sin θ cos φ a 21 =0 a 22 =cos φ a 23 =-sin φ a 31 =-sin θ a 32 =cos θ sin φ a 33 =cos θ cos φ

Claim 10

The system of claim 7 wherein: said means for generating an output signal comprises a solid state control differential transmitter.