The present disclosure provides an unmanned flight system and a control system for an unmanned flight system. The unmanned flight system comprises: a body and a lift mechanism connected to the body, wherein the lift mechanism includes two rotor assembly arm structures respectively provided on two sides of the body, wherein each of the rotor assembly arm structures respectively includes: an arm, a pivotable rotor assembly, a motor for driving the rotor assembly to pivot about a pivot axis, and a motor base for mounting the motor, wherein one end of the arm is pivotally connected to one side of the body, the motor base is pivotally provided on the other end of the arm, and a rotational axis of the motor base is higher than a center of gravity of the unmanned flight system. The unmanned flight system according to the present disclosure can achieve a longer flight time, a simple rotor assembly structure, and easier overall assembly and maintenance.
UNMANNED FLIGHT SYSTEM AND CONTROL SYSTEM FOR USE IN UNMANNED FLIGHT SYSTEM
UNBEMANNTES FLUGSYSTEM UND STEUERUNGSSYSTEM ZUR VERWENDUNG IN EINEM UNBEMANNTEN FLUGSYSTEM
SYSTÈME DE VOL SANS ÉQUIPAGE ET SYSTÈME DE COMMANDE POUR UTILISATION DANS LE SYSTÈME DE VOL SANS ÉQUIPAGE
2022-02-23
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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