Neural network procedures were explored with the objectives to control a delta wing in the non-linear domain. Results show that neural networks are well suited to represent non-linear computed lift and pressure forces on delta wings. A model problem, the flare maneuver, suggests that neural network controllers can perform well for non-linear systems provided that suitable input and training data are provided to it.


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    Titel :

    Thrust-Induced Effects on a Pitching-Up Delta Wing Flow Field: Control of Stalled Wings


    Beteiligte:
    L. VanDommelen (Autor:in)

    Erscheinungsdatum :

    1995


    Format / Umfang :

    5 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch