Abstract Design of the Korea Lunar Pathfinder Orbiter (KPLO) attitude control subsystem is a unique challenge that requires refined models that simulate the cis-lunar and lunar orbital environments including coordinate frame changes, and a new sun-pointing control mode that satisfies Sun and communication pointing constraints. This paper introduces LUNASIM, a simulator for verifying the attitude control performance of KPLO. The simulation architecture is described, and attitude control performance verification results of the sun-pointing control sub-mode are presented.


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    Titel :

    Attitude Control Simulator for the Korea Pathfinder Lunar Orbiter


    Beteiligte:
    Jung, Dawoon (Autor:in) / Kwon, Jae Wook (Autor:in) / Baek, Kwangyul (Autor:in) / Ahn, Han Woong (Autor:in)


    Erscheinungsdatum :

    2019-01-01


    Format / Umfang :

    12 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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