Roll measuring device

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

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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:
patent: 3312423 (1967-04-01), Welch
patent: 3439170 (1969-04-01), Zagote et al.
patent: 3451643 (1969-06-01), Sargent et al.
patent: 3568954 (1971-03-01), McCorkle
patent: 3746281 (1973-07-01), Stripling
patent: 4027399 (1977-06-01), Armstrong
patent: 4054254 (1977-10-01), Cole
patent: 4063366 (1977-12-01), Bane
patent: 4159577 (1979-07-01), Bergkvist
patent: 4163325 (1979-08-01), Hughes
patent: 4168813 (1979-09-01), Pinson et al.
patent: 4172994 (1979-10-01), Bergkvist
patent: 4253242 (1981-03-01), McInerney
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).

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