Hybrid multi-objective orbit-raising optimization with operational constraints
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DOI: 10.1016/j.actaastro.2020.05.022
Abstract: Abstract The optimal design of orbit raising trajectories is formulated within a multi-objective hybrid optimal control framework. The spacecraft can be equipped with chemical, electric or combined chemical-electric propulsion systems. The model incorporates realistic effects… read more here.
Keywords: multi objective; objective orbit; hybrid multi; orbit ... See more keywords