Single actuator direct drive roll control

Aeronautics and astronautics – Missile stabilization or trajectory control – Stabilized by rotation

Reexamination Certificate

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C244S003100, C102S501000

Reexamination Certificate

active

06848648

ABSTRACT:
A system and method for controlling roll in a projectile. The novel system (56) includes first (52) and second (58) sections adapted to counter-rotate relative to each other and a mechanism (76) for inducing the counter-rotation to generate a roll torque on the projectile (50). In the preferred embodiment, the mechanism (76) is a motor comprised of a rotor (64) affixed to the first section (52), and the second section (58) which acts as a stator that rotates around the rotor (64) when a current is applied to the armature. In an alternative embodiment, the second section (58) is turned by a motor (80) attached to the first section (52) which drives a small gear engaging a full-diameter ring gear (82) on the second section (58). In the illustrative examples, the first (52) and second (58) sections are a missile forebody and a tail section of the projectile.

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patent: 6646242 (2003-11-01), Berry et al.
patent: 11 41 537 (1962-12-01), None

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