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Published in 2018 at "Acta Astronautica"
DOI: 10.1016/j.actaastro.2018.01.032
Abstract: Abstract This paper investigates the dynamic characteristics a three-body tethered satellite system in large elliptic orbits and the control strategy to suppress the libration of the system in orbital transfer process. The system is modeled…
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Keywords:
system large;
system;
body tethered;
control ... See more keywords