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Calculating method of series for true anomaly of a spacecraft elliptic orbit - MaRDI portal

Calculating method of series for true anomaly of a spacecraft elliptic orbit

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Publication:957645

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DOI10.1007/BF03246249zbMath1170.70380MaRDI QIDQ957645

Xiaoqin Gu, Zhaoyang Tan

Publication date: 1 December 2008

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Mathematics Subject Classification ID

Orbital mechanics (70M20) Dynamical systems in numerical analysis (37N30)

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