Abstract The previous chapters have discussed the orbital prediction technology, inertial navigation and initial alignment technologies, inertial/satellite integrated navigation technology, inertial/starlight integrated navigation technology, inertial device redundant fault tolerance and fault reconfiguration technology, and guidance and midcourse correction technology of the OTV. During the whole process of flight mission of OTV, the technologies described in these chapters will be involved. Thus, the chapter takes the example of OTV sending the payloads into Earth synchronous orbit to make one integrated description of the technical applications in the chapters.


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    Titel :

    Orbital Control Strategy


    Beteiligte:
    Li, Xuefeng (Autor:in) / Li, Chaobing (Autor:in)


    Erscheinungsdatum :

    2018-01-01


    Format / Umfang :

    12 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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