Abstract When the OTV is at medium high orbit, the navigation satellite signal received by the receiver is relatively weak, even unavailable at certain period. At this moment, the INS/GNSS-integrated navigation technology described in the previous chapter could not be used for improving the accuracy of inertial navigation.


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    Titel :

    INS/CNS-Integrated Navigation Technology


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


    Erscheinungsdatum :

    01.01.2018


    Format / Umfang :

    15 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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