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Published in 2017 at "Iet Control Theory and Applications"
DOI: 10.1049/iet-cta.2017.0176
Abstract: In this study, the problem of robust control for spacecraft rendezvous on elliptical orbit, which contains parameter uncertainties and external disturbances, is investigated based on the implicit Lyapunov function method. A state-feedback controller is first…
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Keywords:
spacecraft rendezvous;
elliptical orbit;
robust control;
control ... See more keywords