Modeling Halo Orbits and the Associated Manifolds in the Restricted Three Body Problem

Development of halo orbits and their associated invariant manifolds are investigated. Halo orbits play a fundamental role in complex space mission designs. In essence, halo orbits are periodic solutions of the restricted three body problem (R3BP) determined under specific initial conditions. In this...

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Bibliographic Details

Published in:	فصلنامه علوم و فناوری فضایی
Main Authors:	M. Jafari Nadoushan, S. H. Pourtakdoust
Format:	Article
Language:	Persian
Published:	Aerospace Research Institute 2010-06-01
Subjects:	restricted three body problem halo orbits stable and unstable manifolds differential correction technique
Online Access:	https://jsst.ias.ir/article_14403_c435d59c0d48a2e1ae1d05001a3d59ec.pdf