Stabilized transportation machine

Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance

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Details

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

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