Analytical solutions to the four post-Newtonian effects in a near-Earth satellite orbit

DOI10.1007/BF00052615zbMath0775.70036OpenAlexW1963723093MaRDI QIDQ1194805

Lin Liu, Cheng Huang

Publication date: 4 October 1992

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

Full work available at URL: https://doi.org/10.1007/bf00052615

Mathematics Subject Classification ID

Relativistic dynamics for problems in Hamiltonian and Lagrangian mechanics (70H40) Orbital mechanics (70M20)

Related Items (8)

Measuring the perigee advance of an artificial satellite under the angular momentum and Earth's electromagnetic field influence ⋮ The equations of motion of the joint effects of the relativistic and solar radiation pressure on an Earth artificial satellite. ⋮ The post-Newtonian effects in the critical inclination problem in artificial satellite theory ⋮ Canonical solution of the critical inclination problem taking into account PN-corrections ⋮ Analytical treatment of the relativistic and solar radiation pressure effects on an artificial satellite ⋮ Relativistic satellite orbits: central body with higher zonal harmonics ⋮ Numerical integration of relativistic equations of motion for Earth satellites ⋮ The relativistic and direct solar radiation pressure effects on an axially symmetric spacecraft. I: The Hamiltonian and the canonical equations of motion.

Cites Work

• Relativistic effects for near-Earth satellite orbit determination
• Relativistic effects in the motion of artificial satellites: The oblateness of the central body. II
• The two-body problem in the (truncated) PPN ? Theory
• Unnamed Item

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