A piloted simulation study was performed in the Cockpit Motion Facility at the National Aeronautics and Space Administration Langley Research Center. The research was motivated by the desire to reduce the commercial transport airplane fatal accident rate due to in-flight loss of control. The purpose of this study, which focused on a generic T-tail transport airplane, was to assess pilot sensitivity to flight dynamics model formulation used during a simulator stall recognition and recovery training/demonstration profile. To accomplish this, the flight dynamics model was designed with many configuration options. The model options were based on recently acquired static and dynamic stability and control data from sources that included wind tunnel, water tunnel, and computational fluid dynamics. The results, which are specific to a transport airplane stall recognition and recovery guided demonstration scenario, showed the two most important aerodynamic effects (other than stick pusher) to model were stall roll- off and the longitudinal static stability characteristic associated with the pitch break.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Pilot Sensitivity to Simulator Flight Dynamics Model Formulation for Stall Training


    Beteiligte:

    Kongress:

    AIAA SciTech Forum 2019 ; 2019 ; San Diego, CA, United States


    Erscheinungsdatum :

    2019-01-07


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Pilot Sensitivity to Simulator Flight Dynamics Model Formulation for Stall Training

    Cunningham, Kevin / Shah, Gautam H. / Murphy, Patrick C. et al. | AIAA | 2019


    Flight Simulator Augmentation for Stall and Upset Training

    Gingras, D. / Ralston, J. / Oltman, R. et al. | British Library Conference Proceedings | 2014


    PILOT TRAINING DEVICE FOR VIRTUAL FLIGHT SIMULATOR

    CHO YEONG IL | Europäisches Patentamt | 2024

    Freier Zugriff

    Post-stall Flight Model Fidelity Effects on Full Stall Recovery Training

    Grant, Peter R. / Moszczynski, Gregory J. / Schroeder, Jeffery A. | AIAA | 2018


    Flight simulator co-pilot

    Gulick, Charles | SLUB | 1986