Earth Escape Trajectories Starting from L2 Point-Reference-Cited by-同舟云学术

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Earth Escape Trajectories Starting from L2 Point

Published:2006-06-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA/AAS Astrodynamics Specialist Conference and Exhibit
language:
Short-container-title:

Author:

Nakamiya Masaki¹,Yamakawa Hiroshi²

Affiliation:

1. The Graduate University for Advanced Studies

2. Japan Aerospace Exploration Agency

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-6751

Reference15 articles.

1. February,2004.

2. TransitionsinCelestial Mechanics,"Chaos,Vol.10,No.2,June2000,p.p.427-469.

3. Body Problem and Space Mission Design," Proceedings of AIAA/AAS Astrodynamics Specialist Meeting, Quebec City, Canada, August,2001,AAS01-301.

4. 4Ross,S.D.,Koon,W.S.,Lo,M.W.,Marsden,J.E.,andMasdemont,J."ApplicationofDynamicalSystemsTheorytoaVery LowEnergy Transfer,"AAS/AIAASpaceFlightMechanicsConference,Maui,8-12 February,2004.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Escape Trajectories from the L2 Point of the Earth-Moon System;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2014

2. Preliminary Analysis of Space Transportation Systems with Spaceports Around Libration Points;AIAA Guidance, Navigation and Control Conference and Exhibit;2008-06-15

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