An aircraft control system includes: a first engine attached to an airframe of an aircraft; a second engine attached to the airframe; a first power generator connected to an engine shaft of the first engine; a second power generator connected to an engine shaft of the second engine; an electric motor driven with electric power supplied from one or both of the first power generator and the second power generator; a rotor driven with a driving force output from the electric motor; and a controller configured to estimate whether noise excess conditions have been satisfied on the basis of information for estimating noise and to change one or both of a rotation speed and a magnitude of a torque such that noise is lower than that before the noise excess conditions have been satisfied when it is estimated that the noise excess conditions have been satisfied.


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    Title :

    AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD, AND STORAGE MEDIUM


    Contributors:

    Publication date :

    2023-07-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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