Improved Two-Impulse Transfer to Halo Orbits in Earth-Moon Elliptic Restricted Three Body Problem Framework Using Differential Evolution (AAS 20-607)
AAS/AIAA Astrodynamics Specialist Conference ; 2020 ; Online
Astrodynamics 2020 ; Part 5 ; 4945-4964
2021
Aufsatz (Konferenz)
Englisch
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