On-board flight control panel system

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

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Details

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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patent: 3343767 (1967-09-01), Cafissi
patent: 4033525 (1977-07-01), Leonard et al.
patent: 4175491 (1979-11-01), Thomanek

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