Aeronautics and astronautics – Missile stabilization or trajectory control – Remote control
Patent
1985-06-20
1987-05-05
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Remote control
244 321, F42B 1502
Patent
active
046625801
ABSTRACT:
A method for compensating for pre-reentry errors generated by the weapon ivery system to provide a reduced impact range error dispersion over that provided by a ballistic trajectory after reentry comprising maneuvering the reentry body after reentry so that the terminal flight direction is essentially in line with the line of means of the reentry body's position-error ellipse that exists just prior to reentry. The reentry body trajectory follows a sequence of a ballistic leg from reentry, a dive maneuver including an optional pullup leg and a pulldown leg to establish the required terminal direction, and a terminal ballistic leg to impact. The required maneuvering is accomplished by modulating the aerodynamic lift of the reentry body by controlling the reentry body's roll orientation.
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Beers R. F.
Curry C. D. B.
Daubenspeck W. C.
Jordan Charles T.
The United States of America as represented by the Secretary of
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