This paper details the design of the cislunar optical navigation system being proposed for the Orion Earth-Moon (EM) missions. In particular, it presents the mathematics of the navigation filter. The unmodeled accelerations and their characterization are detailed. It also presents the analysis that has been performed to understand the performance of the proposed system, with particular attention paid to entry flight path angle constraints and the delta-V performance.


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    Titel :

    Navigation Design and Analysis for the Orion Earth-Moon Mission


    Beteiligte:

    Kongress:

    AAS/AIAA Space Flight Mechanics Conference ; 2014 ; Santa Fe, NM, United States


    Erscheinungsdatum :

    2014-01-26


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Navigation Design and Analysis for the Orion Earth-Moon Mission (AAS 14-263)

    D Souza, C. / Zanetti, R. / American Institute of Aeronautics and Astronautics, | British Library Conference Proceedings | 2014




    Observability Analysis and Filter Design for the Orion Earth–Moon Attitude Filter

    Zanetti, Renato / D’Souza, Christopher N. | AIAA | 2015


    Orion Optical Navigation Progress Toward Exploration: Mission 1

    Holt, Greg N. / D'Souza, Christopher N. / Saley, David | NTRS | 2018