Optimal Low-Thrust Trajectories Using Nonsingular Equinoctial Orbit Elements (IAA-AAS-SciTech2018-044 — AAS 18-834)
IAA/AAS SciTech Forum on Space Flight Mechanics and Space Structures and Materials ; 1. ; 2018 ; Moskau
2020
Conference paper
English
Optimal low-thrust rendezvous using equinoctial orbit elements
Online Contents | 1996
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