Abstract
Autonomous navigation for spacecraft in large elliptical orbit refers to that the spacecraft can determine its parameter on orbit in real time, independent on measurement and control of ground station. Once in-orbit spacecraft navigate autonomously, it decreases the dependence on ground station and greatly improves the viability. Even in such bad situation that the tracking measurement on the ground has been interrupted over a period of time, the spacecraft could keep the continuity of the tasks.
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Li Yong, Wei Chunling. Review on the Development of Autonomous Navigation Techniques for Satellites [J]. Space Control, 2005, 20(2): 70–74.
Tan Longyu, Kang Guohua, Chen Shaohua. A navigation scheme for high-altitude long endurance unmanned aerial vehicle based on magnetic survey [J]. Sichuan ordnance Journal, 2012, 33(2): 4–8.
Tan Longyu, Kang Guohua, Zhang Yuchun. Research on INS/GPS integrated navigation scheme assist by geomagnetism [C]. The fourth China Information Fusion Conference, 2012.
Peng Yang, He Liang, Han Fei. Study on short time data mutation of autonomous celestial navigation sensor [C]. Chinese CCC Control Conference, 2013.
Yang Wenbo, He Liang, Han Fei. An improved autonomous navigation filtering algorithm for LEO Spacecraft under weak constellation signals[C]. Shanghai inertial society academic exchange meeting, 2012.
Yang Wenbo. Autonomous navigation method of high orbit spacecraft based on GNSS [C]. Shanghai Institute of Astronautics, 2012.
YANG Wenbo. Adaptive Autonomous Navigation Method for HEO Satellite Based on Multi-Constellation Information [C]. 14thISCOPS, 2014.
Fang Jancheng, Ning Xiaolin, Tian Yulong. Principle and method of autonomous celestial navigation for spacecraft [M]. National Defense Industry Press, 2006.
Hicks D K,Wiesel J. Autonomous Orbit Determination System for Earth Satellites [J]. Journal of Guidance, Control and Dynamics, 1998, 15(3): 562–566.
Robert Gounley, Robert White, Eliezer Gai. Autonomous Satellite Navigation by Stellar Refraction. Guidance and Control Conference [C],1983, 359–367.
Wang Guangjun. Star sensor and its star map processing technology [D]. Postdoctoral standing out report of Beijing University of Aeronautics and Astronautics, 2005.
Zhang Limin, Xiong Zhi, Yu Feng. Orbit determination of microsatellite based on pseudo range of GPS [J]. Chinese Space Science and Technology, 2008, 27(4): 30–33.
Zhang Limin, Xiong Zhi, Qiao Li. Accuracy analysis on satellite autonomous navigation using radar altimeter and attitude sensors [J]. Transducer and Microsystem Technologies, 2008, 27(4).
Hua Bing, Liu Jianye, Xiong Zhi. Federal Filtering Algorithm in SINS/Beidou/STAR Integrated Navigation System [J]. Journal of Applied Science, 2006, 24(2): 120–124.
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Liu, F., Lu, S., Sun, Y. (2019). Autonomous Navigation Technology of Whole Space. In: Guidance and Control Technology of Spacecraft on Elliptical Orbit. Navigation: Science and Technology. Springer, Singapore. https://doi.org/10.1007/978-981-10-7959-7_4
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DOI: https://doi.org/10.1007/978-981-10-7959-7_4
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