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Proceedings Paper

Decision-making method for small space aircraft navigation based on information fusion
Author(s): Weidong Wang; Jiaqi Liu; Peng Liu; Lei Mu
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Paper Abstract

A decision-making method of navigation for the small spacecraft is proposed. Attitude information is obtained by microelectromechanical gyroscope and geomagnetism sensor. Kalman filter and other information fusion techniques are used to improve the navigation accuracy. The long-term on-orbit navigation control of small aircraft is realized, reducing the cost of on-orbit navigation.

Paper Details

Date Published: 25 October 2017
PDF: 8 pages
Proc. SPIE 10463, AOPC 2017: Space Optics and Earth Imaging and Space Navigation, 1046309 (25 October 2017); doi: 10.1117/12.2283022
Show Author Affiliations
Weidong Wang, National Key Lab. of Science and Technology (China)
Beijing Institute of Space Long March Vehicle (China)
Jiaqi Liu, National Key Lab. of Science and Technology (China)
Beijing Institute of Space Long March Vehicle (China)
Peng Liu, National Key Lab. of Science and Technology (China)
Beijing Institute of Space Long March Vehicle (China)
Lei Mu, National Key Lab. of Science and Technology (China)
Beijing Institute of Space Long March Vehicle (China)


Published in SPIE Proceedings Vol. 10463:
AOPC 2017: Space Optics and Earth Imaging and Space Navigation
Carl Nardell; Suijian Xue; Huaidong Yang, Editor(s)

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