Nonlinear Attractive and Reachable Sets Under Optimal Control in Three-Body Problem
Author:
Affiliation:
1. Kyushu University, Fukuoka 819-0395, Japan
2. University of Colorado at Boulder, Boulder, Colorado 80309
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003334
Reference24 articles.
1. Application of Dynamical Systems Theory to Trajectory Design for a Libration Point Mission
2. GómezG.LlibreJ.MartnezR.SimóC., Dynamics and Mission Design Near Libration Point Orbits—Volume 1: Fundamentals: The Case of Collinear Libration Points, World Scientific, Singapore, 2001, pp. 143–188.
3. Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
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