Paper
2 September 2003 New method for the autonomous celestial navigation of lunar explorer based on the unscented Kalman filter
Jiancheng Fang, Yu Zhang
Author Affiliations +
Proceedings Volume 5253, Fifth International Symposium on Instrumentation and Control Technology; (2003) https://doi.org/10.1117/12.522116
Event: Fifth International Symposium on Instrumentation and Control Technology, 2003, Beijing, China
Abstract
Celestial Navigation is a completely autonomous navigation method for spacecraft. When the Extended Kalman filter is applied to the autonomous celestial navigation, the state and measurement equations need to be linearized. The precision of the estimation isn't fine because of the truncated error of the high-order items introduced by linearization. Unscented Kalman filtering is a new method aimed at nonlinear systems. It is applied to the autonomous celestial navigation of the lunar explorer in this paper, and the simulation is studied based on the Cartesian coordinates. The results demonstrate that the characteristic of the Unscented Kalman filtering is superior to the Extended Kalman filter.
© (2003) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Jiancheng Fang and Yu Zhang "New method for the autonomous celestial navigation of lunar explorer based on the unscented Kalman filter", Proc. SPIE 5253, Fifth International Symposium on Instrumentation and Control Technology, (2 September 2003); https://doi.org/10.1117/12.522116
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Cited by 3 scholarly publications.
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KEYWORDS
Filtering (signal processing)

Electronic filtering

Navigation systems

Nonlinear filtering

Star sensors

Complex systems

Sensors

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