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.
Cite
CITATION STYLE
APA
Li, X., & Li, C. (2018). Ins/cns-integrated navigation technology. In Navigation: Science and Technology (pp. 73–87). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-10-6334-3_6
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