Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1985-07-25
1987-07-07
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F42B 15027
Patent
active
046781420
ABSTRACT:
A small diameter, 20 mm to 50 mm, guided projectile is used in antiaircraft defense. A pulsing laser designator illuminates the target aircraft. Energy reflected from the aircraft is received by the guided projectile. The guided projectile is fired from a standard weapon but the spining caused by the riflings are removed before active tracking and guidance occurs. The received energy is focused by immersion optics onto a bridge cell. AC coupling and gating removes background and allows steering signals to move extended vanes by means of piezoelectric actuators in the rear of the guided projectile.
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Collier Stanton E.
Jordan Charles T.
Singer Donald J.
The United States of America as represented by the Secretary of
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