Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1973-08-10
1985-04-23
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 324, F42B 1328, F42B 1502
Patent
active
045125376
ABSTRACT:
Control is provided to conventional gun-fired projectiles by substituting for the standard fuze thereof a device comprising a canard frame and a main housing, which threads into the fuze well of the projectile, with the canard frame being rotatable with respect to the main housing and having deflectable canards thereon for providing vernier correction on the trajectory to the projectile.
REFERENCES:
patent: 3000307 (1961-09-01), Trotter, Jr.
patent: 3065931 (1962-11-01), Dixon et al.
patent: 3067681 (1962-12-01), Beman
patent: 3072055 (1963-01-01), Ross
patent: 3072365 (1963-01-01), Linscott et al.
patent: 3111088 (1963-11-01), Fisk
patent: 3154015 (1964-10-01), Muller
patent: 3455243 (1969-07-01), Martin
patent: 3711040 (1973-01-01), Carver
Nussdorfer Theodore J.
Sands Timothy B.
Sebestyen George
Sinclair Ronald R.
Smith John A.
Etlinger Louis
Jordan Charles T.
Sanders Associates Inc.
Seligman Richard I.
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