Keplerian motion and gyration

DOI10.1007/BF01371329zbMath0384.70019MaRDI QIDQ4164887

M. Vitins

Publication date: 1978

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

Mathematics Subject Classification ID

Stability for problems in linear vibration theory (70J25) Celestial mechanics (70F15) Motion of the gyroscope (70E05) Stability theory for ordinary differential equations (34Dxx)

Related Items (5)

Motion of artificial satellites in the set of Eulerian redundant parameters. III ⋮ Orbit computations with the Eulerian topological regular elements with oblateness ⋮ Error bounds for perturbation methods ⋮ Uniform formulation for orbit computation: the intermediate elements ⋮ Attitude dynamics of a rigid body in Keplerian motion

Cites Work

• Unnamed Item
• Unnamed Item
• Accurate integration of geostationary orbits with Burdet's focal elements
• The geometry of the orbits of artificial satellites
• Accurate computation of highly eccentric satellite orbits
• Virtual singularities in the artificial satellite theory
• A Mathematical Theory of the Orbits About an Oblate Planet
• The main problem of artificial satellite theory for small and moderate eccentricities
• Numerical stabilization of the differential equations of Keplerian motion
• Qualitative properties of orbits about an oblate planet

This page was built for publication: Keplerian motion and gyration