Two methods of combining multiple response types into a single flexible command model are provided and include receiving a pilot stick input, generating an aircraft response to the pilot stick input that is a continuous blend of response types by including calculable time-varying coefficients set as a function of a magnitude of the pilot stick input and other aircraft states such as airspeed, imposing at least an angular acceleration command limit and using other non-linear elements to optimize the aircraft response to the pilot stick input.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Flexible command model for aircraft control


    Beteiligte:

    Erscheinungsdatum :

    2018-10-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    FLEXIBLE COMMAND MODEL FOR AIRCRAFT CONTROL

    GREENFIELD AARON L / WITTMER KENNETH S | Europäisches Patentamt | 2020

    Freier Zugriff

    FLEXIBLE COMMAND MODEL FOR AIRCRAFT CONTROL

    GREENFIELD AARON L / WITTMER KENNETH S | Europäisches Patentamt | 2017

    Freier Zugriff


    COMMAND CENTRE FOR MANUAL CONTROL OF AIRCRAFT

    PCHENTLESHEV VALERIJ TURKUBEEVICH | Europäisches Patentamt | 2021

    Freier Zugriff

    Command augmentation control laws for maneuvering aircraft

    STENGEL, R. / BROUSSARD, J. / BERRY, P. | AIAA | 1977