A linear solution of the equations of motion of an earth-orbiting satellite based on a Lie-series

DOI10.1007/BF01232196zbMath0531.70011MaRDI QIDQ3313330

Dieter J. Lelgemann

Publication date: 1983

Published in: Celestial Mechanics (Search for Journal in Brave)

zbMATH Keywords

satellite theoryLie-seriesEarth-orbiting satellite

Mathematics Subject Classification ID

Hamilton's equations (70H05) Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (2)

Radial, transverse and normal satellite position perturbations due to the geopotential ⋮ A First Order Automated Lie Transform

Cites Work

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