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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft Model for the Aiaa Controls Design Challenge


    Beteiligte:

    Erscheinungsdatum :

    1991


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft Model for the AIAA Controls Design Challenge

    Brumbaugh, R.W. | Online Contents | 1994





    Linear and nonlinear aircraft flight control for the AIAA Controls Design Challenge

    WISE, KEVIN / DIERKS, MICHAEL / KERKEMEYER, BRUCE et al. | AIAA | 1992