A note on ?The main problem of satellite theory for small eccentricities, by A. Deprit and A. Rom, 1970?

DOI10.1007/BF01230328zbMath0219.70013OpenAlexW2023704386MaRDI QIDQ5624727

Kaare Aksnes

Publication date: 1971

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

Full work available at URL: https://doi.org/10.1007/bf01230328

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (6)

Exact Delaunay normalization of the perturbed Keplerian Hamiltonian with tesseral harmonics ⋮ Solution to the main problem of the artificial satellite by reverse normalization ⋮ Mean values of particular functions in the elliptic motion ⋮ A new radial, natural, higher-order intermediary of the main problem four decades after the elimination of the parallax ⋮ Brouwer's satellite solution redux ⋮ Analytical theory of earth's artificial satellites (A.T.E.A.S.)

Cites Work

• The main problem of artificial satellite theory for small and moderate eccentricities

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