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.


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    Title :

    AIRCRAFT


    Contributors:
    WERNER CARSTEN (author) / CHALAS UWE (author)

    Publication date :

    2015-12-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge



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