Orbit calculations near by the equilibrium points by a discrete mechanics method

DOI10.1007/BF01230398zbMath0465.70028OpenAlexW1982947587MaRDI QIDQ3917553

Jerzy Albrycht, Andrzej Marciniak

Publication date: 1981

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

Full work available at URL: https://doi.org/10.1007/bf01230398

zbMATH Keywords

equilibrium pointsEarth-Moon systemorbit calculationsdiscrete mechanics methodrotating frame of references

Mathematics Subject Classification ID

Celestial mechanics (70F15) Orbital mechanics (70M20) Software, source code, etc. for problems pertaining to mechanics of particles and systems (70-04)

Related Items (2)

Arbitrary order numerical solutions conserving the Jacobi constant in the motion near the equilibrium points ⋮ Discrete Hill's equations

Cites Work

• NEW FORMS OF DISCRETE MECHANICS
• An algebraic, energy conserving formulation of classical molecular and Newtonian 𝑛-body interaction
• Unnamed Item
• Unnamed Item
• Unnamed Item

This page was built for publication: Orbit calculations near by the equilibrium points by a discrete mechanics method