Guided projectile system

Claim 2

A guided projectile system for guiding a projectile to a target, said system comprising: a tracking and guidance system comprising: a target tracker; a projectile tracker for providing a projectile-tracking signal; a target designator for designating the target using a target-tracking signal, and for providing range data indicative of the range to the target; and a processor coupled to the target designator, the target tracker, and the projectile tracker for processing target and projectile return signals and target range signals to generate an actuator command signal that is transmitted by the projectile tracker to the projectile that is used to alter the flight of the projectile; and wherein the projectile includes a projectile reference and control system that comprises: an optical reference including polarized and unpolarized retroreflectors for reflecting the projectile-tracking signal back to the projectile tracker; a detector that is responsive to the projectile-tracking signal provided by the projectile tracker, for detecting the actuator command signal transmitted by the projectile tracker; a command operated actuator coupled to the detector for processing the actuator command signal and to produce a trajectory modification signal that is used to alter the flight of the projectile; and a divert assembly coupled to the command operated actuator for generating thrust that diverts the trajectory of the projectile in response to the trajectory modification signal; and wherein the optical reference is caused to nutate while the projectile flies towards the target, and wherein the tracking and guidance system initially measures roll orientation of the projectile by monitoring the nutation of the polarized return signal while the projectile is relatively close to the projectile tracker, and subsequently measures roll orientation of the projectile by monitoring the modulation of the polarized return signal from the projectile tracker when the projectile is further from the projectile tracker, wherein continued rotation of the projectile allows continued measurement of its roll orientation.

Claim 3

The system of claim 1 wherein the target tracker comprises an imaging tracker.

Claim 4

The system of claim 1 wherein the target tracker comprises a laser designator return signal tracker.

Claim 5

The system of claim 1 wherein the projectile tracker comprises a high repetition rate pulsed laser illuminator.

Claim 6

The system of claim 1 wherein the projectile tracker comprises an amplitude modulated continuous wave laser.

Claim 7

The system of claim 1 wherein the projectile comprises a spin stabilized projectile.

Claim 8

The system of claim 1 wherein the projectile comprises an aerodynamically stabilized projectile.

Claim 9

The system of claim 7 wherein target tracker provides a projectile-tracking laser beam at a first operating wavelength and wherein the projectile tracker provides a second laser beam operating at a different wavelength from the projectile-tracking laser beam, and wherein the second laser beam illuminates the polarized retroreflector disposed on the projectile, and wherein the polarization of the second laser beam is continually rotated, and wherein the roll orientation of the projectile is determined by processing the polarized return beams from the polarized and unpolarized retroreflectors.

Claim 10

The system of claim 1 wherein the tracking and guidance system further comprises an encoder for encoding the actuator command signal and wherein the projectile reference and control system further comprises a decoder disposed between the detector and the command operated actuator for decoding the encoded actuator command signal.

Claim 11

The system of claim 1 wherein the target tracker comprises a laser designator tracker that operates at a first operating wavelength and wherein the projectile tracker comprises a laser illuminator that operates at a second operating wavelength that is different from the first operating wavelength.

Claim 12

The system of claim 10 wherein the projectile tracker comprises a laser illuminator whose output energy beam is encoded.

Claim 13

The system of claim 1 wherein the command operated actuator comprises an explosive actuator that is directly ignited by a laser pulse that is focused thereon.

Claim 14

The system of claim 12 wherein the command operated actuator comprises a graded index lens that is used to focus the laser pulse thereon.

Claim 15

The system of claim 1 which comprises a phase locked loop to track the roll position of the projectile as it spins, and wherein input to the phase locked loop at short range are signals that comprise the azimuth and elevation angle of the polarized and unpolarized retroreflectors and the variation in amplitude of the polarized return signal therefrom, and at long range comprises only the polarized return signal, and wherein continuous measurement of roll position resolves ambiguity of the polarized return by locking the phase lock loop to the roll angle of the projectile at short range when nutation unambiguously defines roll position of the projectile.

Claim 16

The system of claim 1 wherein the nutation of the optical reference is resolved using a quadrant detector in the projectile tracker.

Claim 17

A guided projectile system for guiding an aerodynamically stabilized projectile to a target, said system comprising: a tracking and guidance system comprising: a target tracker; a projectile tracker for providing a projectile-tracking signal and which comprises a phase locked loop to track the roll position of the aerodynamically stabilized projectile as it spins; a target designator for designating the target using a target-tracking signal, and for providing range data indicative of the range to the target; and a processor coupled to the target designator, the target tracker, and the projectile tracker for processing target and projectile return signals and target range signals to generate an actuator command signal that is transmitted by the projectile tracker to the aerodynamically stabilized projectile that is used to alter the flight of the projectile; and wherein the aerodynamically stabilized projectile includes a projectile reference and control system that comprises: an optical reference including polarized and unpolarized retroreflectors for reflecting the projectile-tracking signal back to the projectile tracker; a detector that is responsive to the projectile-tracking signal provided by the projectile tracker, for detecting the actuator command signal transmitted by the projectile tracker; a command operated actuator coupled to the detector for processing the actuator command signal and to produce a trajectory modification signal that is used to alter the flight of the aerodynamically stabilized projectile; and a divert assembly coupled to the command operated actuator for generating thrust that diverts the trajectory of the aerodynamically stabilized projectile in response to the trajectory modification signal; and wherein input to the phase locked loop at short range are signals that comprise the azimuth and elevation angle of the polarized and unpolarized retroreflectors and the variation in amplitude of the polarized return signal therefrom, and at long range comprises only the polarized return signal, and wherein continuous measurement of roll position resolves ambiguity of the polarized return by locking the phase lock loop to the roll angle of the projectile at short range when nutation unambiguously defines roll position of the projectile.

Claim 18

A guided projectile system for guiding an aerodynamically stabilized projectile to a target, said system comprising: a tracking and guidance system comprising: a target tracker; a projectile tracker for providing a projectile-tracking signal and which comprises a phase locked loop to track the roll position of the aerodynamically stabilized projectile as it spins; a target designator for designating the target using a target-tracking signal, and for providing range data indicative of the range to the target; and a processor coupled to the target designator, the target tracker, and the projectile tracker for processing target and projectile return signals and target range signals to generate an actuator command signal that is transmitted by the projectile tracker to the aerodynamically stabilized projectile that is used to alter the flight of the projectile; and wherein the aerodynamically stabilized projectile includes a projectile reference and control system that comprises: an optical reference including polarized and unpolarized retroreflectors for reflecting the projectile-tracking signal back to the projectile tracker; a detector that is responsive to the projectile-tracking signal provided by the projectile tracker, for detecting the actuator command signal transmitted by the projectile tracker; a command operated actuator coupled to the detector for processing the actuator command signal and to produce a trajectory modification signal that is used to alter the flight of the aerodynamically stabilized projectile; and a divert assembly coupled to the command operated actuator for generating thrust that diverts the trajectory of the aerodynamically stabilized projectile in response to the trajectory modification signal; and wherein input to the phase locked loop at short range are signals that comprise the azimuth and elevation angle of the polarized and unpolarized retroreflectors and the variation in amplitude of the polarized return signal therefrom, and at long range comprises only the polarized return signal, and wherein continuous measurement of roll position resolves ambiguity of the polarized return by locking the phase lock loop to the roll angle of the projectile at short range when nutation unambiguously defines roll position of the projectile.