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2018 | OriginalPaper | Chapter

6. INS/CNS-Integrated Navigation Technology

Authors : Xuefeng Li, Chaobing Li

Published in: Navigation and Guidance of Orbital Transfer Vehicle

Publisher: Springer Singapore

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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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previous chapter INS/GNSS Integrated Navigation Technology
next chapter Redundant Fault Tolerance and Failure Reconfiguration Technology of Inertial Devices
Literature
1.
Li Yijie. 2012. Research on Autonomous Navigation Filtering Algorithm of Large Elliptical Orbit Vehicle. Harbin Institute of Technology.
2.
Zhang Cheng. 2012. Research on INS/CNS Integrated Navigation Technology of Aerospace Vehicle. Nanjing University of Aeronautics and Astronautics.
3.
Fang Jiancheng, Ning Xiaolin. 2006. Celestial Navigation Principle and Applications. Beihang University Press.
4.
Zhang Libin. 2010. Rocket Upper-stage Navigation, Research on Midcourse Correction and Attitude Control. Harbin Institute of Technology.
5.
Qian Yingjing. 2013. Research on Autonomous Navigation and Station keeping For Quasi-periodic Orbit in The Earth-Moon System. Harbin Institute of Technology.
6.
Chen Shaohau. 2012. Research on SINS/GPS/CNS Autonomous Navigation Technology of High-orbital Maneuver Vehicle. Nanjing University of Aeronautics and Astronautics.
7.
Zhou Baolin. 2009. Research on Semi-physical Situation of INS/CNS Integrated Navigation System. Harbin Institute of Technology.
8.
Xueyuan, Jian, Ma. Guangfu, and Luo Jing. 2003. Model of Attitude Measurement Error of Infrared Horizon Sensor. Journal of Aerospace 24 (2): 138–143.
9.
Tang Qiong. 2007. Determination of Vehicle Autonomous Orbit Based on Starlight Refraction. Northwestern Polytechnical University.
Metadata
Title
INS/CNS-Integrated Navigation Technology
Authors
Xuefeng Li
Chaobing Li
Copyright Year
2018
Publisher
Springer Singapore
Book
Navigation and Guidance of Orbital Transfer Vehicle

Print ISBN: 978-981-10-6333-6

Electronic ISBN: 978-981-10-6334-3

Copyright Year: 2018

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

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