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Preliminary space mission design under uncertainty

Croisard, Nicolas and Vasile, Massimiliano and Kemble, Stephen and Radice, Gianmarco (2010) Preliminary space mission design under uncertainty. Acta Astronautica, 66 (5-6). pp. 654-664. ISSN 0094-5765

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    Abstract

    This paper proposes a way to model uncertainties and to introduce them explicitly in the design process of a preliminary space mission. Traditionally, a system margin approach is used in order to take the min to account. In this paper, Evidence Theory is proposed to crystallise the inherent uncertainties. The design process is then formulated as an optimisation under uncertainties(OUU). Three techniques are proposed to solve the OUU problem: (a) an evolutionary multi-objective approach, (b) a step technique consisting of maximising the belief for different levels of performance, and (c) a clustering method that firstly identifies feasible regions.The three methods are applied to the Bepi Colombo mission and their effectiveness at solving the OUU problem are compared.

    Item type: Article
    ID code: 29016
    Notes: Impact Factor 0.609, Half-Life 6.9
    Keywords: modelling uncertainties, optimisation under uncertainties (OUU), BepiColombo mission, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Aerospace Engineering
    Subjects: Technology > Mechanical engineering and machinery
    Technology > Motor vehicles. Aeronautics. Astronautics
    Department: Faculty of Engineering > Mechanical and Aerospace Engineering
    Related URLs:
    Depositing user: Pure Administrator
    Date Deposited: 21 Mar 2011 11:36
    Last modified: 05 Sep 2014 23:46
    URI: http://strathprints.strath.ac.uk/id/eprint/29016

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