| 摘要 |
The invention relates to a vertical takeoff and landing aircraft (101) for transporting persons or loads, comprising a plurality of preferably equivalent and redundant electric motors (3) and propellers (2), substantially arranged in one surface, wherein each propeller is assigned an individual electric motor to drive the propeller, said aircraft being characterised in that at least one position sensor is provided for the position control of the aircraft (101) in a signal-operative connection to at least one signal processing unit which is designed or set up to automatically perform the position control with due regard to measurement data from the position sensor by regulating the speed of at least some of the electric motors (3), preferably with a signal-operative effect on the speed controller assigned to each electric motor such that the aircraft (101) is positioned in space with the surface defined by the propeller (2) substantially horizontal at all times, without control input by a pilot or a remote control. |
