Dynamics of Solar Radiation Pressure–Assisted Maneuvers Between Lissajous Orbits
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
2. Polytechnic University of Catalonia, 08028 Barcelona, Spain
3. Barcelona University, 08007 Barcelona, Spain
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.G003725
Reference33 articles.
1. GordonS. C. “Orbit Determination Error Analysis and Comparison of Station-Keeping Costs for Lissajous and Halo-Type Libration Point Orbits and Sensitivity Analysis Using Experimental Design Techniques,” NASA N93-24721, 1993, pp. 395–409.
2. Numerical determination of Lissajous trajectories in the restricted three-body problem
3. Study of the transfer from the Earth to a halo orbit around the equilibrium pointL 1
4. Low Energy Transit Orbits in the Restricted Three-Body Problems
5. Heteroclinic connections between periodic orbits and resonance transitions in celestial mechanics
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