Centrifugally operated moving-mass roll control system

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

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F41G 700

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045778124

ABSTRACT:
A roll control system for a reentry vehicle having the pay load positioned within the vehicle so as to offset the center of gravity from the aerodynamic axis of the vehicle. A radial mass unbalance is created in the aft end of the vehicle to create a trim angle of attack dependent upon the vehicle roll rate which provides a source of roll torque with the out-of-plane radial center of mass offset. With the use of a mass and spring arrangement, the mass unbalance is controlled by centrifugal force to terminate the roll torque at the prescribed design roll rate.

REFERENCES:
patent: 3437286 (1969-04-01), Lindley
patent: 3690596 (1972-09-01), Durran et al.
patent: 3767139 (1973-10-01), Fischell

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