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Published in 2025 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2024.3513956
Abstract: To enhance the analytical guidance for the powered descent with multiple constraints, a guidance method using a tunable segmented acceleration profile is developed. With three segments and 12 tunable parameters, the acceleration profile is successively…
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Keywords:
guidance;
acceleration profile;
using tunable;
guidance method ... See more keywords