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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    Title :

    Mars Reconnaissance Orbiter design approach for high-resolution surface imaging


    Contributors:
    Skulsky, E. D. (author) / Lee, S. W. (author)

    Publication date :

    2003-02-05


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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