A high-fidelity simulation of a conceptual Mars Ascent Vehicle has been developed for end-to-end performance evaluation. The simulation environment is the Dynamics Simulator for Entry, Descent and Surface landing (DSENDS). The simulation work includes the modeling of the multi-body components, Martian environment, flight software and mission timeline. Using this simulation environment, the end-to-end MAV flight performance is evaluated, both in the nominal scenario and in perturbed off-nominal scenarios where model uncertainties are taken into account.


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    Titel :

    Hybrid propulsion Mars Ascent Vehicle concept flight performance analysis


    Beteiligte:
    Benito, Joel (Autor:in) / Noyes, Connor (Autor:in) / Shotwell, Robert (Autor:in) / Karp, Ashley (Autor:in) / Nakazono, Barry (Autor:in) / Singh, Gurkirpal (Autor:in) / Kim, Hunjoo (Autor:in) / Schoenenberger, Mark (Autor:in) / Korzun, Ashley (Autor:in) / Lobbia, Marcus (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.03.2017


    Format / Umfang :

    1341124 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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