Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1973-11-28
1976-03-02
Pendegrass, Verlin R.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
73 1E, G01C 2500
Patent
active
039413454
ABSTRACT:
A radial arm tracker with a constant drive ratio for use in monitoring the osition of a guidance platform during the firing azimuth alignment phase. One end of the radial arm is mounted to the rotor of an encoder and a telescope is pivotally mounted at the free end of the radial arm through a constant ratio drive system to a stator of an encoder. The stator of the encoder is coupled to a north seeking device. The missile firing azimuth is referenced to the output of the north seeking device through the radial arm tracker.
REFERENCES:
patent: 3797782 (1974-03-01), Stripling et al.
Hunter Joe S.
Stripling William W.
White Harold V.
Deaton James T.
Edelberg Nathan
Gibson Robert P.
Pendegrass Verlin R.
The United States of America as represented by the Secretary of
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