Control systems for moving bodies

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

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Details

244 321, F42B 1060

Patent

active

054234972

ABSTRACT:
A missile or other moving body comprising a rotatable portion arranged for rotation relative to another portion of the missile or body and control means for rotating said rotatable portion to bring it to any one of a plurality of preselected positions in relation to a datum and for exerting a thrust thereon having a lateral component with respect to the axis of rotation of said rotatable portion to produce a steering effect on the missile or body, said control means including a variable-incidence control surface mounted on the rotatable portion for rotation about a rotary axis transverse to the rotary axis of the rotatable portion, and actuator means responsive to control signals applied thereto for turning said control surface about its rotary axis to a first disposition in which it produces a component thrust causing rotation of said rotatable portion, and a second disposition in which it produces a lateral steering force on the missile.

REFERENCES:
patent: 3010677 (1961-11-01), Guthrie et al.
patent: 3067681 (1962-12-01), Beman
patent: 3111088 (1963-11-01), Fisk

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