Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1974-07-11
1977-01-25
Pendegrass, Verlin R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 712
Patent
active
040047547
ABSTRACT:
A missile disposed for operation from a launch pad to impinge on a target th electromagnetic rays emanating therefrom includes a seeker for direction of the rays impinging thereon in patterns for alignment therewith and means for directing the missile to the target responsive to the alignment.
REFERENCES:
patent: 2948813 (1960-08-01), Osborne
patent: 3076095 (1963-01-01), Becklund et al.
patent: 3235733 (1966-02-01), Dauguet
patent: 3297395 (1967-01-01), Dardarian
patent: 3756538 (1973-09-01), McLean
Cox Mary V.
Widner Rayburn K.
Deaton James T.
Edelberg Nathan
Gibson Robert P.
Pendegrass Verlin R.
The United States of America as represented by the Secretary of
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