Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1975-05-08
1985-02-19
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 722
Patent
active
045000514
ABSTRACT:
A cannon launched guided projectile having a gyro based electro-optical target finding and guidance system which includes an optical system carried by a gyro to provide target location information for an electronic system to produce gyro rotor torquing signals and for producing projectile guidance signals from gyro pickoff outputs is disclosed. The electronics system includes two difference channels for processing pitch and yaw signals responsive to the electrical output of a light detector and a sum channel for controlling the two difference channels responsive to target acquisition and master trigger signals.
REFERENCES:
patent: 3756538 (1973-09-01), McLean
patent: 3920200 (1975-11-01), Evans et al.
patent: 4003655 (1977-01-01), Wasilko
patent: 4006356 (1977-02-01), Johnson et al.
patent: 4009393 (1977-02-01), Ashley, Jr. et al.
patent: 4009848 (1977-03-01), Albert et al.
patent: 4010365 (1977-03-01), Meyers et al.
Cottle, Jr. Wilbur W.
Smith Lilburn R.
Bandy Alva H.
Heiting Leo N.
Jordan Charles T.
Sharp Melvin
Texas Instruments Incorporated
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