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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    Title :

    A mathematical simulation model of a 1985-era tilt-rotor passenger aircraft


    Contributors:

    Publication date :

    1976-08-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English