Control augmentation system for flight vehicles

Details Control augmentation system for flight vehicles Control augmentation system for flight vehicles

1978-10-13

1980-04-15

Blix, Trygve M.

Aeronautics and astronautics

Aircraft control

Automatic

244 1713, 244178, 364434, B64C 1304

Patent

active

041980174

ABSTRACT:
A control augmentation system for stabilization and control of flight vehes, wherein control of vehicle angular velocities in proportion to control input is effected, and where stabilization of the corresponding vehicle attitude is also effected. The system consists of both feedforward and feedback signal paths. The feedback paths provide augmentation of the vehicle's inherent stability. The feedforward paths augment the controllability factors available to the pilot. The control augmentation system is a solution to hingeless rotor control problems.

REFERENCES:
patent: 3175786 (1965-03-01), Frank
patent: 3711042 (1973-01-01), Rempfer
patent: 3733039 (1973-05-01), O'Connor
patent: 4109886 (1978-08-01), Tribken

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