Numerical calculations in the orbital determination of an artificial satellite for a long arc

DOI10.1007/BF00692873zbMath0825.70097OpenAlexW2087734167MaRDI QIDQ1341867

Lin Liu, Xin-Hao Liao

Publication date: 6 February 1995

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

Full work available at URL: https://doi.org/10.1007/bf00692873

Mathematics Subject Classification ID

Computational methods for problems pertaining to mechanics of particles and systems (70-08) Orbital mechanics (70M20)

Related Items (3)

Computation of quasiclassical trajectories by symplectic algorithm for the \(N(^4S)+O_2(X^3\Sigma^-_g)\to NO(X^2\Phi)+O(^3P)\) reaction system ⋮ The adjustment-stabilization method for constrained systems ⋮ Effects of manifold correction methods on chaos indicators

Cites Work

• Non-two-body reference orbit for Encke's method.
• Unnamed Item
• Unnamed Item

This page was built for publication: Numerical calculations in the orbital determination of an artificial satellite for a long arc