Control systems for moving bodies

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

Patent

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Details

F42B 1060

Patent

active

053930118

ABSTRACT:
Disclosed herein is a missile having a rotatable portion arranged for rotation relative to another portion of the missile which contains spacedly mounted electromagnetic coils for respectively operating first and second control member actuator mechanisms for controlling the missile.

REFERENCES:
patent: 3067681 (1962-12-01), Beman
patent: 3111088 (1963-11-01), Fisk
patent: 3154015 (1964-10-01), Muller

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