This study was motivated by a need to develop a reliable method of predicting the agility characteristics of various aircraft. To fully investigate the agility of an aircraft, maneuvers which push the limits of an aircraft's maneuvering capabilities must be simulated. In these cases, classic trajectory optimization techniques either require too many assumptions for a realistic solution or require a good guess of the final solution before the problem is even attempted. This study investigated both the utility of pseudospectral optimization methods for robust trajectory optimization as well as the potential for demonstrating differences in aircraft agility characteristics of several specific maneuvers. Three variations of a basic F-16 mathematical model were simulated for various maneuvers specifically designed to demonstrate aircraft maneuvering limits.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Demonstrative Maneuvers for Aircraft Agility Predictions


    Beteiligte:
    D. M. Hall (Autor:in)

    Erscheinungsdatum :

    2008


    Format / Umfang :

    112 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Demonstrative Maneuvers for Aircraft Agility Prediction

    Hall, David / Shearer, Christopher | AIAA | 2008


    Demonstrative Maneuvers for Aircraft Agility Prediction

    Hall, D. / Shearer, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    Aircraft agility maneuvers

    CLIFF, EUGENE / THOMPSON, BRIAN | AIAA | 1992


    Aircraft agility maneuvers

    Cliff, Eugene M. / Thompson, Brian G. | NTRS | 1992


    Nonlinear Decoupling Control and Aircraft Agility Maneuvers

    Zhou, Z. Q. / Gao, H. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1994