In this paper, we present a novel integrated simulation tool that models science yield and mission resources as a function of science payload, mission and system design, spacecraft behavior and modes, and target uncertainties. This provides a comprehensive and self-consistent approach to multi-spacecraft mission formulation around small bodies. We demonstrate this tool for the case of a notional three-spacecraft mission to the near-Earth asteroid Apophis, which will flyby Earth in 2029.


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    Titel :

    Integrated Science and Engineering Simulation Environment for Formation Flying Mission around Small Body


    Beteiligte:
    Bandyopadhyay, Saptarshi (Autor:in) / Amini, Rashied (Autor:in) / Miller, Robert (Autor:in) / Bhaskaran, Shyam (Autor:in) / Anderson, Rodney L. (Autor:in) / Hernandez, Sonia (Autor:in) / Haynes, Mark (Autor:in) / Adell, Philippe (Autor:in) / Raymond, Carol (Autor:in) / Fesq, Lorraine (Autor:in)


    Erscheinungsdatum :

    2023-03-04


    Format / Umfang :

    9107548 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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