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INS/CNS-Integrated Navigation Technology

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Navigation and Guidance of Orbital Transfer Vehicle

Part of the book series: Navigation: Science and Technology ((NASTECH))

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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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Reference Documentation

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Author information

Authors and Affiliations

  1. Beijing Aerospace Automatic Control Institute, Beijing, China

    Xuefeng Li & Chaobing Li

Authors
  1. Xuefeng Li
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  2. Chaobing Li
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Correspondence to Xuefeng Li .

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© 2018 Springer Nature Singapore Pte Ltd. and National Defense Industry Press, Beijing

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Cite this chapter

Li, X., Li, C. (2018). INS/CNS-Integrated Navigation Technology. In: Navigation and Guidance of Orbital Transfer Vehicle. Navigation: Science and Technology. Springer, Singapore. https://doi.org/10.1007/978-981-10-6334-3_6

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  • DOI: https://doi.org/10.1007/978-981-10-6334-3_6

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  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-6333-6

  • Online ISBN: 978-981-10-6334-3

  • eBook Packages: EngineeringEngineering (R0)

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