Electro-mechanical roll control apparatus and method

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

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Details

244 324, F42B 1002, F42B 1024, F42B 1014

Patent

active

054528640

ABSTRACT:
An apparatus and method for controlling roll of a projectile is disclosed. The projectile includes two sections decoupled about a roll axis. The front section includes a stator and the rear section includes a rotor and a static spin imparting member. The spin rate of the projectile is controlled by utilizing the rotor and stator in combination as a generator to brake the spin or as a motor to establish spin.

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