Aeronautics and astronautics – Missile stabilization or trajectory control – Externally mounted stabilizing appendage
Patent
1996-09-30
1998-07-07
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Externally mounted stabilizing appendage
244 321, 244 323, 244 326, F42B 1000, F41G 700
Patent
active
057756368
ABSTRACT:
A guided artillery projectile is provided for use in improving its accuracy while spinning. The projectile includes an artillery shell, a plurality of movable fins, fin actuators for two-dimensional steering, a fin control for the fin actuators, and a guidance unit for the fin control. A method of guiding an artillery projectile is also provided.
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Hollis, Michael S.L., "Preliminary Design of a Range Correction Module for n Artillery Schell", Army Research Laboratory Report ARL-MR-298, Mar. 1996.
Vig John R.
Waugh Steven W.
Jordan Charles T.
The United States of America as represented by the Secretary of
Wesson Theresa M.
Zelenka Michael
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