Optimal Control of Endoatmospheric Launch Vehicle Systems: Geometric and Computational Issues
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DOI: 10.1109/tac.2019.2929099
Abstract: In this paper, we develop a geometric analysis and a numerical algorithm, based on indirect methods, to solve optimal guidance of endoatmospheric launch vehicle systems under mixed control-state constraints. Two main difficulties are addressed. First,… read more here.
Keywords: control; optimal control; launch vehicle; endoatmospheric launch ... See more keywords