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.
INS/CNS-Integrated Navigation Technology
01.01.2018
15 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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