TY - JOUR
T1 - Analysis of medium-energy transfers to the Moon
AU - Oshima, Kenta
AU - Topputo, Francesco
AU - Campagnola, Stefano
AU - Yanao, Tomohiro
N1 - Funding Information:
This study has been partially supported by Grant-in-Aid for JSPS Fellows No. 15J07090, and by JSPS Grant-in-Aid No. 26800207.
Publisher Copyright:
© 2016, Springer Science+Business Media Dordrecht.
PY - 2017/3/1
Y1 - 2017/3/1
N2 - This study analyzes a recently discovered class of exterior transfers to the Moon. These transfers terminate in retrograde ballistic capture orbits, i.e., orbits with negative Keplerian energy and angular momentum with respect to the Moon. Yet, their Jacobi constant is relatively low, for which no forbidden regions exist, and the trajectories do not appear to mimic the dynamics of the invariant manifolds of the Lagrange points. This paper shows that these orbits shadow instead lunar collision orbits. We investigate the dynamics of singular, lunar collision orbits in the Earth–Moon planar circular restricted three-body problem, and reveal their rich phase space structure in the medium-energy regime, where invariant manifolds of the Lagrange point orbits break up. We show that lunar retrograde ballistic capture trajectories lie inside the tube structure of collision orbits. We also develop a method to compute medium-energy transfers by patching together orbits inside the collision tube and those whose apogees are located in the appropriate quadrant in the Sun–Earth system. The method yields the novel family of transfers as well as those ending in direct capture orbits, under particular energetic and geometrical conditions.
AB - This study analyzes a recently discovered class of exterior transfers to the Moon. These transfers terminate in retrograde ballistic capture orbits, i.e., orbits with negative Keplerian energy and angular momentum with respect to the Moon. Yet, their Jacobi constant is relatively low, for which no forbidden regions exist, and the trajectories do not appear to mimic the dynamics of the invariant manifolds of the Lagrange points. This paper shows that these orbits shadow instead lunar collision orbits. We investigate the dynamics of singular, lunar collision orbits in the Earth–Moon planar circular restricted three-body problem, and reveal their rich phase space structure in the medium-energy regime, where invariant manifolds of the Lagrange point orbits break up. We show that lunar retrograde ballistic capture trajectories lie inside the tube structure of collision orbits. We also develop a method to compute medium-energy transfers by patching together orbits inside the collision tube and those whose apogees are located in the appropriate quadrant in the Sun–Earth system. The method yields the novel family of transfers as well as those ending in direct capture orbits, under particular energetic and geometrical conditions.
KW - Bicircular restricted four-body problem
KW - Circular restricted three-body problem
KW - Collision orbits
KW - Levi-Civita regularization
KW - Medium-energy transfer
KW - Retrograde ballistic capture orbits
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U2 - 10.1007/s10569-016-9727-7
DO - 10.1007/s10569-016-9727-7
M3 - Article
AN - SCOPUS:84986327411
SN - 0923-2958
VL - 127
SP - 285
EP - 300
JO - Celestial Mechanics and Dynamical Astronomy
JF - Celestial Mechanics and Dynamical Astronomy
IS - 3
ER -