Aeronautics and astronautics – Missile stabilization or trajectory control – Automatic guidance
Patent
1984-11-07
1987-10-13
Jordan, Charles T.
Aeronautics and astronautics
Missile stabilization or trajectory control
Automatic guidance
244 328, F42B 1502
Patent
active
046993339
ABSTRACT:
A missile on-board pitch, yaw and roll flight control panel system, the system having a plurality of control panels operated by an actuator drive. The edge of the control panels slanted so when the panels are in an open position, clockwise and counter clockwise roll of the missile can be controlled.
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Jordan Charles T.
The Boeing Company
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