An optimal control approach has been used to model pilot performance during STOL flare and landing. The model is used to predict pilot landing performance for three STOL configurations, each having a different level of automatic control augmentation. Model predictions are compared with flight simulator data. It is concluded that the model can be effective design tool for studying analytically the effects of display modifications, different stability augmentation systems, and proposed changes in the landing area geometry.


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    Titel :

    A predictive pilot model for STOL aircraft landing


    Beteiligte:

    Erscheinungsdatum :

    01.03.1974


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    A predictive pilot model for STOL aircraft landing

    Kleinman, David L. / Killingsworth, William R. | TIBKAT | 1974




    Arrested Landing Studies for STOL Aircraft

    Chen-Chung Hsin | AIAA | 1974