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Published in 2025 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2024.3497872
Abstract: The problem of guiding a constant thrust vehicle to achieve lunar orbit with optimal fuel consumption is the focus of this article. The computational cost of the optimal guidance law remains a challenge for onboard…
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Keywords:
guidance;
guidance quasi;
optimal guidance;
lunar ... See more keywords