MULTI-ROTOR AIRCRAFT AND METHOD OF CONTROLLING SAME
We propose a method of controlling a multi-rotor aircraft (1), said aircraft (1) comprising at least four lifting rotors (2; R1-R6), each having a first rotation axis which is essentially parallel to a yaw axis (z) of the aircraft (1), and at least one forward propulsion device (3), the at least one...
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Sprache: | eng ; fre ; ger |
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