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.


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    Title :

    Structural dynamics, stability, and control of helicopters


    Contributors:

    Publication date :

    1976-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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