Spacecraft attitude control provides the basic stability so that sensors, solar panels, antennas and other hardware are properly oriented to perform their functions. A Horizon scanner can automatically seek the earth horizon by detecting the sharp discontinuity in InfraRed intensity at the outer edge of the Earth's mesopause for purposes of a spacecraft's orientation and control.As a satellite in a Low Earth Orbit (LEO) and three-axis stabilized, the Canadian satellite RADARSAT-1 is equipped with two horizon scanners (HS) in order to scan dynamically across the Earth's disc and to establish the attitude relative to the Earth. This paper discusses the thermal design and analyzes the on-orbit thermal performance of the HS.


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    Titel :

    Analysis of Thermal Design and On-Orbit Performance of the Horizon Scanners of RADARSAT-1


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Nikanpour, Darius (Autor:in) / Wang, Guanghan (Autor:in) / Deraspe, Guy (Autor:in) / Nappert, Stephane (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 2003



    Erscheinungsdatum :

    07.07.2003




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Analysis of Thermal Design and On-Orbit Performance of the Horizon Scanners of RADARSAT-1

    Wang, G. / Nikanpour, D. / Deraspe, G. et al. | British Library Conference Proceedings | 2003


    On-Orbit Thermal Performance of RADARSAT-1 Spacecraft

    Nikanpour, D. / Showalter, D. / Wang, G. | SAE Technical Papers | 2001


    On-Orbit Thermal Performance of RADARSAT-1 Spacecraft

    Wang, G. / Nikanpour, D. / Showalter, D. et al. | British Library Conference Proceedings | 2001


    Geometric theory of horizon scanners

    FANG, B. T. | AIAA | 1975


    Geometric theory of horizon scanners

    Fang, B. T. | NTRS | 1975