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Controlling the eccentricity of polar lunar orbits with low-thrust propulsion

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Publication:966234
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DOI10.1155/2009/159287zbMath1184.70012OpenAlexW2128410770WikidataQ58648883 ScholiaQ58648883MaRDI QIDQ966234

B. E. Eshmatov

Publication date: 23 April 2010

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://eudml.org/doc/222833



Mathematics Subject Classification ID

Celestial mechanics (70F15)


Related Items (5)

Permanent magnet Hall thruster development for future Brazilian space missions ⋮ Planetary satellite orbiters: applications for the Moon ⋮ Some orbital characteristics of lunar artificial satellites ⋮ Semianalytic integration of high-altitude orbits under lunisolar effects ⋮ Searching for orbits with minimum fuel consumption for station-keeping maneuvers: an application to lunisolar perturbations




Cites Work

  • Introduction to celestial mechanics




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