Minimizing eclipses via synodic resonant orbits with applications to EQUULEUS and MMX

被引:0
作者
Chikazawa, Takuya [1 ]
Baresi, Nicola [2 ]
Campagnola, Stefano [3 ]
Ozaki, Naoya [4 ]
Kawakatsu, Yasuhiro [4 ]
机构
[1] The University of Tokyo, Tokyo,113-8654, Japan
[2] Surrey Space Centre, University of Surrey, Surrey,GU27XH, United Kingdom
[3] Jet Propulsion Laboratory, California Institute of Technology, Pasadena,CA,91109, United States
[4] Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Kanagawa,252-5210, Japan
来源
Acta Astronautica | 2021年 / 180卷
关键词
Compilation and indexing terms; Copyright 2024 Elsevier Inc;
D O I
暂无
中图分类号
学科分类号
摘要
Deep space missions - Driving parameters - Ephemeris model - Optimal orbit insertion - Periodic trajectories - Power constraints - Resonant orbits - Three-body systems
引用
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页码:679 / 692
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