DocumentCode :
3450793
Title :
Translunar low-energy trajectories via Earth-Moon L1 Lyapunov orbit
Author :
Li, Maodeng ; Jing, Wuxing
Author_Institution :
Dept. of Aerosp. Eng., Harbin Inst. of Technol., Harbin
fYear :
2007
fDate :
15-18 Dec. 2007
Firstpage :
941
Lastpage :
945
Abstract :
This paper is concerned with low-energy Earth- Moon transfer trajectory via Lyapunov orbit located on Earth- Moon libration point LI. The circular restricted three-body problem is used as the model for Earth-Moon system, and Birkhoff regularization is used to avoid singularities when the distance between spacecraft and primary is very short. Using both analytical and numerical methods, Lyapunov orbits near the collinear libration point LI in CR3BP are computed. Stable and unstable manifolds of LI Lyapunov orbit are generated. Finally, Optimized trajectory solutions were found using genetic algorithm between low earth/lunar orbit and stable/unstable manifolds of Lyapunov orbit.
Keywords :
Earth; Lyapunov methods; Moon; aerospace control; astronomy; genetic algorithms; position control; space vehicles; Birkhoff regularization; CR3BP; collinear libration point LI; earth-moon LI Lyapunov orbit; earth-moon libration point LI; genetic algorithm; translunar low energy trajectories; Angular velocity; Biomimetics; Earth; Equations; Fuels; Genetic algorithms; Manifolds; Moon; Orbital robotics; Space vehicles; Birkhoff regularization; Lyapunov orbit; circular restricted three-body problem; genetic algorithm;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Robotics and Biomimetics, 2007. ROBIO 2007. IEEE International Conference on
Conference_Location :
Sanya
Print_ISBN :
978-1-4244-1761-2
Electronic_ISBN :
978-1-4244-1758-2
Type :
conf
DOI :
10.1109/ROBIO.2007.4522290
Filename :
4522290
Link To Document :
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