Systems and methods provide for the evaluation of flight controls for an aerial vehicle and define a vehicle dynamics model corresponding to an aerial vehicle. One or more barrier functions are constructed based on the defined vehicle dynamics model, and candidate invariant sets are identified for the defined vehicle dynamics model using the one or more barrier functions. A plurality of flight controls of the aerial vehicle are analyzed using the identified candidate invariant sets and within the analyzed candidate invariant sets, command tracking of the aerial vehicle is confirmed with control commands, using the analyzed plurality of flight controls. Control commands falling outside of the analyzed candidate invariant sets are identified.


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    Title :

    EVALUATION OF AIR VEHICLE FLIGHT CONTROLS


    Additional title:

    EVALUATION DES COMMANDES DE VOL DE VEHICULE AERIEN



    Publication date :

    2022-09-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / G16Z



    EVALUATION OF AIR VEHICLE FLIGHT CONTROLS

    BYRON NICHOLAS HEERSINK / PAPE MAGUETTE SYLLA / MICHAEL ALTON WARREN | European Patent Office | 2022

    Free access

    EVALUATION OF AIR VEHICLE FLIGHT CONTROLS

    HEERSINK BYRON NICHOLAS / SYLLA PAPE MAGUETTE / WARREN MICHAEL ALTON | European Patent Office | 2022

    Free access

    Flight Controls

    Dryden, Joe Bill | Online Contents | 1994


    Digital flight controls

    Hall, J. C. | NTRS | 1982


    Reentry Vehicle Flight Controls Design Guidelines: Dynamic Inversion

    D. Ito / J. Georgie / J. Valasek et al. | NTIS | 2002