Critical inclination in the main problem of a massive satellite

DOI10.1007/S10569-005-5911-XzbMath1152.70314OpenAlexW2026476318MaRDI QIDQ850673

Antonio Elipe, Sławomir Breiter

Publication date: 6 November 2006

Published in: Celestial Mechanics and Dynamical Astronomy (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10569-005-5911-x

zbMATH Keywords

Analytical methodsCritical inclinationRigid body rotation

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (4)

Frozen orbits at high eccentricity and inclination: application to Mercury orbiter ⋮ Some orbital characteristics of lunar artificial satellites ⋮ Position and velocity perturbations for the determination of geopotential from space geodetic measurements ⋮ Families of first kind periodic solutions of the spatial and planar elliptic restricted three-body problem with collision

Cites Work

• Frozen orbits for satellites close to an Earth-like planet
• Bounds on rotation periods of disrupted binaries in the full 2-body problem
• Stability in the full two-body problem
• The critical inclination in artificial satellite theory
• Canonical transformations depending on a small parameter
• Changes in rotational angular momentum due to gravitational interactions between two finite bodies

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