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Published in 2018 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2018.07.080
Abstract: Abstract The objective of this work is to present a closed-loop guidance algorithm for landing a probe on an irregular shaped rotating asteroid. The main assumption is that the spacecraft is orbiting close to the…
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Keywords:
predictive guidance;
autonomous asteroid;
guidance;
algorithm autonomous ... See more keywords