The InFOC-S X-ray telescope was launched September 16, 2004 aboard a 40 million cubic foot zero pressure high altitude balloon. Its primary objective was to demonstrate advances in hard X-ray focusing optics technology by flying an incident grazing mirror developed in cooperation between NASA Goddard Space Flight Center and Nagoya University, Japan. Launched from Ft. Sumner, NM and recovered near Wickenburg, AZ, the payload successfully collected photons from several X-ray sources during its 27 hour flight at a float altitude of 130,000 feet. To accommodate the instrument's narrow field of view, a precision arc-minute attitude determination and control systems was flown. This paper describes the application of a traditional spacecraft star tracker gyro based attitude determination and control system to the balloon problem. The control system architecture is presented, hardware identified, and software outlined. Simulated results are compared against actual flight data, with recommendations for enhanced performance identified.


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    Titel :

    Up, Up and Away: Arc Minute Pointing at 130,000 Feet


    Beteiligte:
    Freesland, Doug (Autor:in) / Gruner, Timothy (Autor:in) / Olney, Dave (Autor:in) / Bromberg, Bruce (Autor:in) / Collinson, Tom (Autor:in) / Patel, Kiran (Autor:in)

    Kongress:

    AAS Guidance and Control Conference ; 2005 ; Breckenridge, CO, United States


    Erscheinungsdatum :

    01.01.2005


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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