A ganged servo flight control system for an unmanned aerial vehicle is provided. The flight control system may include a swashplate having first, second, and third connection portions; a first control assembly connected to the first connection portion of the swashplate; a second control assembly connected to the second connection portion of the swashplate; and a third control assembly connected to the third connection portion of the swashplate. The first control assembly may include two or more servo-actuators connected to operate in cooperation with each other.
GANGED SERVO FLIGHT CONTROL SYSTEM FOR AN UNMANNED AERIAL VEHICLE
GEKOPPELTES SERVOFLUGSTEUERUNGSSYSTEM FÜR EIN UNBEMANNTES LUFTFAHRZEUG
SYSTÈME DE SERVOCOMMANDE DE VOL COUPLÉ POUR VÉHICULE AÉRIEN SANS PILOTE
2022-01-26
Patent
Elektronische Ressource
Englisch
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