Flight system comprising an aircraft that is equipped with at least four rotors and has a payload, a number of rotors that turn in one direction and a number of rotors that turn in the other direction, and a remote controller. The aircraft is in data-transmitting connection with the remote controller via a transmitter/receiver unit in each case. The aircraft and the remote controller each have a data processing device that is connected to the transmitter/receiver unit, and the aircraft as well as the remote controller have the same sensors for flight position recognition. When there is a change in the angle of the remote controller about its x and/or y and/or z axis, the measure of the change in the angle correlates with a specifiable speed of the aircraft, and the specified speed that corresponds to the change in the angle is transmitted as the setpoint value to the data processing device of the aircraft and/or of the remote controller. The actual value of the speed of the aircraft is determined and compared to the setpoint value in the data processing device. By controlling the rotational speed of the rotors, the thrust is changed until the setpoint value of the speed matches the actual speed of the aircraft.
FLIGHT SYSTEM
MECANISME DE VOL
2015-12-02
Patent
Electronic Resource
English
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