The dynamic synthesis of a helicopter is reported. The method of approach is a variation of the component mode synthesis in the sense that it regards the aircraft as an assemblage of interconnected substructures. The equations of motion are derived in general form by means of the Lagrangian formulation in conjunction with an orderly kinematical procedure that takes into account the superposition of motion of various substructures, thus circumventing constraint problems. (Author)


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    Titel :

    Structural Dynamics, Stability, and Control of Helicopters


    Beteiligte:
    L. Meirovitch (Autor:in) / L. G. Kraige (Autor:in) / A. L. Hale (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    97 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Structural dynamics, stability, and control of helicopters

    Meirovitch, L. / Kraige, L. G. / Hale, A. L. | NTRS | 1976


    Structural Dynamics, Stability, and Control of Helicopters

    Meirovitch, L. / Hale, A. L. | NTRS | 1978


    Stability of helicopters

    De Caria, U. | Engineering Index Backfile | 1931


    Stability and control of tethered helicopters

    Kaufman, L. / Schultz, E.R. | Engineering Index Backfile | 1962


    Inherent Stability of Helicopters

    Crocco, G Arturo | NTRS | 1923