A new technique which converts a constrained optimization problem to an unconstrained one where conflicting figures of merit may be simultaneously considered was combined with a complex mission analysis system. The method is compared with existing single and multiobjective optimization methods. A primary benefit from this new method for multiobjective optimization is the elimination of separate optimizations for each objective, which is required by some optimization methods. A typical wide body transport aircraft is used for the comparative studies.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Aircraft design for mission performance using nonlinear multiobjective optimization methods


    Beteiligte:

    Erscheinungsdatum :

    01.10.1990


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch