One of the objectives of the MRO mission is to use the High-Resolution Imaging Science Experiment (HiRISE) to provide 50 cm/pixel images of future Mars landing sites. To achieve such detail, MRO must meet some very challenging target-relative pointing and pointing stability requirements. A combination of analysis, operational constraints, and spacecraft design modifications were utilized to ensure that the necessary pointing requirements will be met.


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    Titel :

    Mars Reconnaissance Orbiter design approach for high-resolution surface imaging


    Beteiligte:
    Skulsky, E. D. (Autor:in) / Lee, S. W. (Autor:in)

    Erscheinungsdatum :

    2003-02-05


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Mars Reconnaissance Orbiter Design Approach for High-Resolution Surface Imaging (AAS 03-067)

    Lee, S. W. / Skulsky, E. D. / Chapel, J. et al. | British Library Conference Proceedings | 2003


    Mars Reconnaissance Orbiter mission

    Graf, J. / Zurek, R. | NTRS | 2001


    HiRISE: The High Resolution Imaging Science Experiment for Mars Reconnaissance Orbiter

    McEwen, A. S. / Delamere, W. A. / Eliason, E. M. et al. | NTRS | 2002


    Mars Reconnaissance Orbiter Mission

    De Paula, Ramon P. | AIAA | 2003


    Mars Reconnaissance Orbiter Navigation

    You, Tung-Han / Halsell, Allen / Highsmith, Dolan et al. | NTRS | 2004