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Advances in Astronomy
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2019
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Article
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Tab 1
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Research Article
Initial Parameter Analysis about Resonant Orbits in Earth-Moon System
Table 1
Simulation results for the 1:2 resonant orbits when the initial parameters can cause the closest distance to lie within the Moon’s sphere of influence.
Initial Phase
Eccentricity
e
Simulation Results
10°
0.34
Flyby
0.43
Flyby
0.5
Resonance transition
20°
0.43
Flyby
0.5
Flyby
0.55
Resonance transition
30°
0.5
Flyby
0.54
Flyby
0.6
Resonance transition
40°
0.56
Flyby
0.6
Flyby
0.65
Resonance transition
50°
0.61
Flyby
0.67
Flyby
0.71
Resonance transition
60°
0.67
Resonance transition
0.71
Flyby
0.75
Resonance transition
70°
0.72
Resonance transition
0.76
Flyby
0.8
Resonance transition
80°
0.76
Resonance transition
0.8
Flyby
0.84
Resonance transition
90°
0.81
Resonance transition
0.84
Flyby
0.88
Resonance transition
100°
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-