Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1982-07-20
1985-09-17
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 700
Patent
active
045415900
ABSTRACT:
A roll measuring device for missiles comprising an inertia member supported about an axis by a case and provided with means whereby rotation of the case relative to the inertia member about the said axis can be measured, the inertia member being balanced about the axis so as to be rotationally uninfluenced by gravity or movement medial or angular to the axes.
REFERENCES:
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patent: 4262861 (1981-04-01), Goldstein
Avionics, Stellar-Inertial Guidance Reduces Error, by Horsfell, Aviation Week, Mar. 17 (1958), p. 73.
Cochan, Analysis and Design of the Gyroscope, pp. 1-7 and 76-77 (1963).
Jordan Charles T.
The Commonwealth of Australia
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