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Proceedings Paper

Simulation and emulation of orbit parameters of spacecraft based on satellite passive detection
Author(s): Lihua Zhang; Kun Xu; Yuhai Bao; Jijun Li; Lan Yan
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Paper Abstract

The medium-low orbit satellite is used as observation satellite to make parameters estimation and error analysis of the spacecraft orbit. Based on the variable mass particle dynamics, the simplified motion equation of observation satellite was numerically solved by the Runge-Kutta method, and the position of the observation satellite at any time was calculated more accurately. Based on the variable mass particle dynamics, the orbit estimation equation of the spacecraft was given, and the position and the velocity data of the spacecraft at any time were numerically solved by the Runge- Kutta method, and then the fitting curves of these data were obtained. The residual analysis was made to test the output from the model, which indicated that this model is acceptable and valid.

Paper Details

Date Published: 26 January 2016
PDF: 6 pages
Proc. SPIE 9903, Seventh International Symposium on Precision Mechanical Measurements, 99032M (26 January 2016); doi: 10.1117/12.2217511
Show Author Affiliations
Lihua Zhang, Beijing Normal Univ. (China)
Inner Mongolia Normal Univ. (China)
Kun Xu, Inner Mongolia Univ. of Technology (China)
Yuhai Bao, Inner Mongolia Normal Univ. (China)
Jijun Li, Inner Mongolia Univ. of Technology (Mongolia)
Lan Yan, Hohhot Vocational College (China)


Published in SPIE Proceedings Vol. 9903:
Seventh International Symposium on Precision Mechanical Measurements
Liandong Yu, Editor(s)

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