Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1975-02-04
1976-03-30
Feinberg, Samuel
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
74 56B, F41G 700, G01C 1928
Patent
active
039469670
ABSTRACT:
A transportation machine such as a ballistic missile disposed for operation n a linear path is provided with a chassis including an aerate atmosphere and a gyroscopic rotor for development therearound of a pressurized aerate ring and for axial orientation in the linear path. A stabilizer develops signals responsive to differences in pressures between the aerate atmosphere and the pressurized ring for rotation of the chassis to axial coincidence with the rotor responsive to the signals.
REFERENCES:
patent: 2852208 (1958-09-01), Schlesman
patent: 3165282 (1965-01-01), Noyes
patent: 3340740 (1967-09-01), Hall
patent: 3435688 (1969-04-01), Ogren
Bailey Escar L.
Rodgers Aubrey
Widner Rayburn K.
Edelberg Nathan
Feinberg Samuel
Gibson Robert P.
Murphy William P.
The United States of America as represented by the Secretary of
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