;Partial Contents: Mathematical Modeling and its Application for Helicopter Maneuver Flight Based on Inverse Simulation; Nonlinear Vibration of Transversely Isotropic Piezoelectric Rectangular Plate; Expert System for Failure Diagnosing and Fatigue Evaluating about Damage of Lugs in Aircraft; A Converter for Switched Reluctance Generator; Hybrid Fuzzy Logic Control by Combining Slide Model and PI for a Nonlinear Flight Control System; Analysis on Dynamic Mold of Spindle of Internal Grinder Based on BP Neural Network.


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    Titel :

    Journal of Nanjing University of Aeronautics and Astronautics, Volume 35, No. 1, 2003


    Beteiligte:
    L. Dewang (Autor:in)

    Erscheinungsdatum :

    2003


    Format / Umfang :

    118 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch