Disclosed are a quad-rotor control system and a control method thereof. The present invention uses a nine axis inertial navigation device based on a quad-rotor with four motors to measure the posture and motion of a flying object, and controls a modularized controller to improve the performance and efficiency of a system. Thereby, the stability of quad-rotor is increased. The adjustment/control of the quad-rotor can be easily carried out. Especially, the performance of a hovering can be improved.
QUAD-ROTOR POSITION CONTROL SYSTEM AND CONTROL METHOD THEREOF
2015-09-23
Patent
Electronic Resource
Korean
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