Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1973-09-26
1986-03-25
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
F41G 700
Patent
active
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
Jordan Charles T.
Killoren Richard J.
Rusz Joseph E.
Singer Donald J.
The United States of America as represented by the Secretary of
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