The possible motions of a satellite about an oblate planet

DOI10.1007/BF01231101zbMath0518.70014OpenAlexW1996719939MaRDI QIDQ3667988

No author found.

Publication date: 1983

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

Full work available at URL: https://doi.org/10.1007/bf01231101

zbMATH Keywords

two degrees of freedomenergy integralequilibrium solutionstopological propertiesconservativecircular equatorial orbitsHill stableregions of motions of satellite around oblate planet

Mathematics Subject Classification ID

Dynamical aspects of finite-dimensional Hamiltonian and Lagrangian systems (37J99) Celestial mechanics (70F15) Orbital mechanics (70M20)

Related Items (2)

Numerical integration of periodic orbits in the main problem of artificial satellite theory ⋮ Collision orbits in the oblate planet problem

Cites Work

• The effects of integrals on the totality of solutions of dynamical systems
• The Possible Motions of a Rigid Body With One Fixed Point
• Bifurcation points in the planar problem of three bodies

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