A rotorcraft small perturbation linear model is described. Rotor flap, inplane and feathering degrees of freedom, as well as control and augmentation systems are defined in addition to the classical vehicle six degrees of freedom. The primary application was intended to be an analytic tool to assess the handling qualities of a dynamically combined main rotor and body. The modeling method retained the higher frequency response properties which aided in evaluating control and stability augmentation systems.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Rotorcraft Linear Simulation Model. Volume 1: Engineering Documentation


    Beteiligte:
    J. S. Reaser (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    185 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    REXOR Rotorcraft Simulation Model. Volume I. Engineering Documentation

    W. D. Anderson / F. Conner / P. Kretsinger et al. | NTIS | 1976