This paper discusses a precision attitude and control technique for meeting these requirements utilizing a similar architecture that was adopted for the Laboratory of Atmospheric and Space Physics (LASP) SNOE (Student Nitrous Oxide Explorer) spinning spacecraft; SNOE has been operating with its ADCS architecture in low earth orbit (LEO) for over two years.


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    Title :

    Precision ADCS of a spinning spacecraft for the Mars Aeronomy Explorer Mission


    Contributors:

    Conference:

    96th AIAA Aerospace Control and Guidance Systems Committee Meeting ; 2005 ; Hilton Head, SC, United States


    Publication date :

    2005-10-19


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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