A generic, state-of-the-art, high-performance aircraft model, including detailed, full-envelope, nonlinear aerodynamics, and full-envelope thrust and first-order engine response data is described. While this model was primarily developed Controls Design Challenge, the availability of such a model provides a common focus for research in aeronautical control theory and methodology. An implementation of this model using the FORTRAN computer language, associated routines furnished with the aircraft model, and techniques for interfacing these routines to external procedures is also described. Figures showing vehicle geometry, surfaces, and sign conventions are included.


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    Title :

    An aircraft model for the AIAA controls design challenge


    Contributors:

    Conference:

    AIAA GNC Conference ; 1991 ; New Orleans, LA, United States


    Publication date :

    1991-12-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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