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Published in 2018 at "Advances in Space Research"
DOI: 10.1016/j.asr.2018.08.046
Abstract: Abstract This paper presents an improved understanding of the interaction of hybrid optimization method with variable low-thrust trajectory optimization requirements. To analyze fuel-optimal bang-bang control problem, a new version of homotopic algorithm, termed robust homotopic…
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Keywords:
homotopic;
low thrust;
optimization;
approach ... See more keywords