Control systems for moving bodies

F - Mech Eng,Light,Heat,Weapons – 42 – B

Patent

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244/1.5

F42B 15/01 (2006.01)

Patent

CA 1336083

A missile has a rotatable portion 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 to produce a steering effect. The control means includes 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. Actuator means responsive to control signals turns the control surface about its rotary axis to a position to produce a component thrust causing rotation of the rotatable portion.

904308

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