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Cosmic Research

, Volume 56, Issue 2, pp 144–150 | Cite as

Calculation and Study of Limited Orbits around the L2 Libration Point of the Sun–Earth System

  • S. A. Aksenov
  • S. A. Bober
Article
  • 21 Downloads

Abstract

A procedure has been proposed for calculating limited orbits around the L2 libration points of the Sun–Earth system. The motion of a spacecraft in the vicinity of the libration point has been considered a superposition of three components, i.e., decreasing (stable), increasing (unstable), and limited. The proposed procedure makes it possible to correct the state vector of the spacecraft so as to neutralize the unstable component of the motion. Using this procedure, the calculation of orbits around various types of libration points has been carried out and the dependence on the orbit type on the initial conditions has been studied.

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Copyright information

© Pleiades Publishing, Ltd. 2018

Authors and Affiliations

  1. 1.National Research University Higher School of EconomicsMoscowRussia
  2. 2.Space Research InstituteRussian Academy of SciencesMoscowRussia

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