US 5,685,504 AGranted

Guided projectile system

AssigneeHughes Missile Systems Company

InventorsArthur J. Schneider, Kenneth R. Johnson, Henry August, Douglas E. Elerath, Paul D. Shubert

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Abstract

A system for guiding the flight of a projectile to a target. The system comprises a tracking and guidance system, the projectile, and a projectile reference and control system that is part of the projectile. The tracking and guidance system includes a target tracker, a projectile tracker for providing a projectile-tracking laser beam, and a target designator for designating the target using a target-tracking laser beam, and for providing range data indicative of the range to the target. A processor is 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 using the projectile-tracking laser beam and that is used to alter the flight of the projectile. The projectile reference and control system includes an optical reference including polarized and unpolarized retroflectors for reflecting the projectile-tracking laser beam back to the projectile tracker, and a detector that is responsive to the projectile-tracking laser beam provided by the projectile tracker, for detecting the actuator command signal transmitted by the projectile tracker. A command operated actuator is coupled to the detector for processing the actuator command signal and for generating a trajectory modification signal that is used to alter the flight of the projectile. 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.

Claims16

Dependent claims

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.

12 more elements

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.

11 more elements

Dependencies are inferred from the claim text.