High-order resonant orbit manifold expansions for mission design in the planar circular restricted 3-body problem

In recent years, stable and unstable manifolds of invariant objects (such as libration points and periodic orbits) have been increasingly recognized as an efficient tool for designing transfer trajectories in space missions. However, most methods currently used in mission design rely on using eigenv...

Full description

Saved in:
Bibliographic Details
Published in:Communications in nonlinear science & numerical simulation Vol. 97; p. 105691
Main Authors: Kumar, Bhanu, Anderson, Rodney L., de la Llave, Rafael
Format: Journal Article
Language:English
Published: Amsterdam Elsevier B.V 01.06.2021
Elsevier Science Ltd
Subjects:
ISSN:1007-5704, 1878-7274
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Be the first to leave a comment!
You must be logged in first