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


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    Titel :

    ADAPTIVE FLIGHT CONTROLS


    Beteiligte:

    Erscheinungsdatum :

    2020-05-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    ADAPTIVE FLIGHT CONTROLS

    WITTMAAK JR JOHN ROBERT / PETERS RUSSEL C / LOUIS ANDREW VINCENT | Europäisches Patentamt | 2023

    Freier Zugriff

    Flight Controls

    Dryden, Joe Bill | Online Contents | 1994


    Analysis of adaptive neural networks for helicopter flight controls

    Leitner, Jesse / Calise, Anthony / Prasad, J | AIAA | 1995


    Digital flight controls

    Dove, B. | NTRS | 1982


    Hydrofluidic Flight Controls

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