Libration transfer design using patched elliptic three-body models and graphics processing units
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[1] Nitin Arora,et al. Parallel Computation of Trajectories Using Graphics Processing Units and Interpolated Gravity Models , 2015 .
[2] Shane D. Ross,et al. Low Energy Transfer to the Moon , 2001 .
[3] Daniel J. Scheeres,et al. The use of invariant manifolds for transfers between unstable periodic orbits of different energies , 2010 .
[4] Pingyuan Cui,et al. Design and analysis of an extended mission of CE-2: From lunar orbit to Sun–Earth L2 region , 2014 .
[5] J. Junkins,et al. Modified Chebyshev-Picard Iteration Methods for Solution of Initial Value Problems , 2011 .
[6] Hiroshi Yamakawa,et al. Analysis of capture trajectories into periodic orbits about libration points , 2008 .
[7] Kathleen C. Howell,et al. Time-free transfers between libration-point orbits in the elliptic restricted problem , 1992 .
[8] Shane D. Ross,et al. Connecting orbits and invariant manifolds in the spatial restricted three-body problem , 2004 .
[9] Bong Wie,et al. Computational Solutions to Lambert’s Problem on Modern Graphics Processing Units , 2015 .
[10] Geshi Tang,et al. CHANG'E-2 lunar escape maneuvers to the Sun–Earth L2 libration point mission , 2014 .
[11] Rodney L. Anderson,et al. Low-Energy Lunar Trajectory Design: Parker/Low-Energy , 2014 .
[12] Lei Liu,et al. Pre-LOI trajectory maneuvers of the CHANG′E-2 libration point mission , 2012, Science China Information Sciences.
[13] Shijie Xu,et al. Stability of two groups of multi-revolution elliptic halo orbits in the elliptic restricted three-body problem , 2015 .
[14] B. Barden,et al. Application of Dynamical Systems Theory to Trajectory Design for a Libration Point Mission , 1997 .
[15] Benjamin F. Villac,et al. Modified Picard Integrator for Spaceflight Mechanics , 2014 .
[16] Nitin Arora,et al. Global Point Mascon Models for Simple, Accurate, and Parallel Geopotential Computation , 2012 .
[17] Gerard Gómez,et al. Study of the transfer from the Earth to a halo orbit around the equilibrium pointL1 , 1993 .
[18] Pingyuan Cui,et al. Analysis of Two-Impulse Capture Trajectories into Halo Orbits of Sun-Mars System , 2014 .
[19] Shijie Xu,et al. Low-energy transfers to a Lunar multi-revolution elliptic halo orbit , 2015 .