One embodiment is an aircraft (100) including at least one propulsion assembly (115); a cargo area (102) for receiving payload to be transported by the aircraft 9100); and a control system (20) for determining characteristics of the received payload; automatically determining optimal control gains for operating the aircraft (100) including the payload based on the determined payload characteristics; and providing control signals to at least one of the at least one propulsion assembly (115)and a control assembly of the aircraft (100)to control operation of the at least one propulsion assembly (115) in accordance with the determined optimal control gains.


    Access

    Download


    Export, share and cite



    Title :

    ADAPTIVE FLIGHT CONTROLS


    Additional title:

    ADAPTIVE FLUGSTEUERUNGEN
    COMMANDES DE VOL ADAPTATIVES


    Contributors:

    Publication date :

    2023-10-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U



    ADAPTIVE FLIGHT CONTROLS

    WITTMAAK JR JOHN ROBERT / PETERS RUSSELL C / LOUIS ANDREW VINCENT | European Patent Office | 2020

    Free access

    Flight Controls

    Dryden, Joe Bill | Online Contents | 1994


    Digital flight controls

    Dove, B. | NTRS | 1982


    Hydrofluidic Flight Controls

    Posingies, W. M. | SAE Technical Papers | 1970


    Secondary Flight Controls

    George, F. | British Library Online Contents | 2007