A flight system comprising an aircraft equipped with at least four rotors and having a payload, a number of rotors rotating in one direction and a number of rotors rotating in the other direction, as well as a remote control, the aircraft being connected to the remote control, so as to transmit data, via respective transmitter/receiver units, both the aircraft and the remote control having a data processing device connected to the respective transmitter/receiver unit, both the aircraft and the remote control having the same sensors for flight attitude detection, where, when there is an angle change in the remote control around its X- and/or Y- and/or Z-axis, the amount of the angle change correlates with a definable speed of the aircraft, the speed specified according to the angle change being transmitted as a target value of the data processing device of the aircraft and/or of the remote control.
AIRCRAFT
2015-12-03
Patent
Electronic Resource
English
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