A sixth-order accurate scheme for solving two-point boundary value problems in astrodynamics
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[1] L. Fox. The Numerical Solution of Two-Point Boundary Problems in Ordinary Differential Equations , 1957 .
[2] S. Rebay,et al. Numerical solution of two-point boundary value problems , 1990 .
[3] V. Szebehely,et al. Theory of Orbits: The Restricted Problem of Three Bodies , 1967 .
[4] A. Roy,et al. From Newton to Chaos , 1995 .
[5] David L. Richardson,et al. Halo Orbit Formulation for the ISEE-3 Mission , 1979 .
[6] Cesar A. Ocampo,et al. Low-Thrust Variable-Specific-Impulse Transfers and Guidance to Unstable Periodic Orbits , 2005 .
[7] J. Masdemont,et al. The Bicircular Model Near the Triangular Libration Points of the RTBP , 1995 .
[8] Gerard Gómez,et al. Dynamics and Mission Design Near Libration Points: Volume III: Advanced Methods for Collinear Points , 2001 .
[9] J. Stoer,et al. Introduction to Numerical Analysis , 2002 .
[10] Arthur E. Bryson,et al. Applied Optimal Control , 1969 .
[11] J. Masdemont,et al. High-order expansions of invariant manifolds of libration point orbits with applications to mission design , 2005 .
[12] R. Battin. An introduction to the mathematics and methods of astrodynamics , 1987 .
[13] J. Lambert. Numerical Methods for Ordinary Differential Systems: The Initial Value Problem , 1991 .
[14] Kazuyuki Yagasaki,et al. Sun-perturbed earth-to-moon transfers with low energy and moderate flight time , 2004 .