The use of various robust optimization methods to solve engineering problems with environmental parameter uncertainty was investigated. Comparisons were made between a novel multi-objective-based robust optimization formulation and conventional robust regularization-based and aggregation-based methods. The results, performance, and philosophies of each method are discussed. A hypersonic vehicle design problem was used as a test bed for the methods presented here. A focus was put on studying the effect of uncertain roughness-induced boundary-layer transition locations on vehicle controllability. The robust regularization results show that a flat wedgelike vehicle design is best for a worst-case scenario, whereas a pyramidal-shaped vehicle design minimizes the expected detrimental effects on vehicle controllability. The analysis proved that the multi-objective robust optimization method was able to identify these two types of results within an overall set of results while also capturing tradeoffs within the design space.


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    Titel :

    Comparison of Robust Optimization Methods Applied to Hypersonic Vehicle Design


    Beteiligte:
    Ryan, Kevin M. (Autor:in) / Lewis, Mark J. (Autor:in) / Yu, Kenneth H. (Autor:in)

    Erschienen in:

    Journal of Aircraft ; 52 , 5 ; 1510-1523


    Erscheinungsdatum :

    2015-02-06


    Format / Umfang :

    14 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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