Orbital behavior of earth satellites. I, II: Orbits about an oblate spheroid

DOI10.1016/0016-0032(57)90977-8zbMath0151.35302OpenAlexW1977631941MaRDI QIDQ2525575

R. E. Roberson

Publication date: 1957

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0016-0032(57)90977-8

zbMATH Keywords

mechanics

Related Items (6)

The critical inclination in artificial satellite theory ⋮ Oblateness correction to impact points of ballistic rockets ⋮ Satellite orbits about a planet with rotational symmetry ⋮ A geometrical derivation of the satellite equations ⋮ Delaunay normalisations ⋮ Delaunay normalisations

Cites Work

• Gravitational torque on a satellite vehicle
• Perturbations of a Satellite's Orbit Due to the Earth's Oblateness
• Unnamed Item

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