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Published in 2020 at "Microgravity Science and Technology"
DOI: 10.1007/s12217-020-09822-y
Abstract: The paper proposes algorithms for controlling the orbital motion of a small spacecraft for executive bodies with constant and variable thrust. The developed algorithms are aimed at neutralizing the influence of temperature shock on the…
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Keywords:
motion small;
technological spacecraft;
spacecraft;
development control ... See more keywords