Paper
25 October 2017 Decision-making method for small space aircraft navigation based on information fusion
Weidong Wang, Jiaqi Liu, Peng Liu, Lei Mu
Author Affiliations +
Proceedings Volume 10463, AOPC 2017: Space Optics and Earth Imaging and Space Navigation; 1046309 (2017) https://doi.org/10.1117/12.2283022
Event: Applied Optics and Photonics China (AOPC2017), 2017, Beijing, China
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.
© (2017) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Weidong Wang, Jiaqi Liu, Peng Liu, and Lei Mu "Decision-making method for small space aircraft navigation based on information fusion", Proc. SPIE 10463, AOPC 2017: Space Optics and Earth Imaging and Space Navigation, 1046309 (25 October 2017); https://doi.org/10.1117/12.2283022
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KEYWORDS
Magnetism

Sensors

Information fusion

Gyroscopes

Microelectromechanical systems

Magnetic sensors

Filtering (signal processing)

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