Modelling of innovative aircraft such as UAVs, X-wing, tilt body and delta-wing is not easy. This paper presents a nonlinear system identification method for modelling air vehicles of complex configuration. This approach is demonstrated through a laboratory helicopter. Extensive time and frequency-domain model-validation tests are employed to instil confidence in the estimated model. The estimated model has a good predictive capability and can be utilized for nonlinear flight simulation studies. The approach presented is suitable for modelling new generation air vehicles.


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    Titel :

    Nonlinear modelling of a twin rotor MIMO system using radial basis function networks


    Beteiligte:
    Ahmad, S.M. (Autor:in) / Shaheed, M.H. (Autor:in) / Chipperfield, A.J. (Autor:in) / Tokhi, M.O. (Autor:in)


    Erscheinungsdatum :

    01.01.2000


    Format / Umfang :

    631728 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch