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.


    Access

    Download


    Export, share and cite



    Title :

    Evaluation of air vehicle flight controls



    Publication date :

    2024-10-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS



    EVALUATION OF AIR VEHICLE FLIGHT CONTROLS

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

    Free access

    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


    Reentry Vehicle Flight Controls Design Guidelines: Dynamic Inversion

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