On-board flight control drag actuator system

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

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Details

102384, 102388, 244 328, F42B 1502, F42B 2524

Patent

active

046244247

ABSTRACT:
A missile on-board flight pitch, yaw and roll control drag actuator system. The system having a plurality of control panels operated by an actuator drive. The actuator drive accurately positioning the panels in a desired position in the airstream of the missile for controlling the flight, orientation and speed of the aircraft.

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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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