1–3 von 3 Ergebnissen
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    Aeroelastic stability of smart trailing-edge flap helicopter rotors

    Shen, J. / Chopra, I. | Tema Archiv | 2001
    eigenanalysis of these homogeneous equations using a constant coefficient approximation approach and the Floquet method. The baseline correlation of ...
    Schlagwörter: intelligenter Werkstoff

    Trailing edge flap control methodology for vibration reduction of helicopter with dissimilar blades

    Roget, B. / Chopra, I. / Gessow, A. | Tema Archiv | 2001
    the proposed methodology lies in its ability to control each rotor blade separately and optimally taking into account blade-to-blade ...

    Detection of helicopter rotor system simulated faults using neural networks

    Ganguli, R. / Chopra, I. / Haas, D.J. | Tema Archiv | 1996
    approach in space and time. Selected helicopter rotor faults are simulated through changes in inertial, damping and stiffness properties of the ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA) , Reston