A mathematical model for use in real-time piloted simulation of a 1985-era tilt rotor passenger aircraft is presented. The model comprises the basic six degrees-of-freedom equations of motion, and a large angle of attack representation of the airframe and rotor aerodynamics, together with equations and functions used to model turbine engine performance, aircraft control system and stability augmentation system. A complete derivation of the primary equations is given together with a description of the modeling techniques used. Data for the model is included in an appendix.


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    Titel :

    A Mathematical Simulation Model of a 1985-Era Tilt-Rotor Passenger Aircraft


    Beteiligte:
    M. A. Mcveigh (Autor:in) / C. A. Widdison (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    244 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch