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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    Title :

    INS/CNS-Integrated Navigation Technology


    Contributors:
    Li, Xuefeng (author) / Li, Chaobing (author)


    Publication date :

    2018-01-01


    Size :

    15 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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