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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    Title :

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


    Contributors:

    Publication date :

    1995


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English