Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft
نویسندگان
چکیده
منابع مشابه
Multi-Objective Robust H∞ Control of Spacecraft Rendezvous
Based on the relative motion dynamic model illustrated by C-W equations, the problem of robust H1 control for a class of spacecraft rendezvous systems is investigated, which contain parametric uncertainties, external disturbances and input constraints. An H1 state-feedback controller is designed via a Lyapunov approach, which guarantees the closed-loop system to meet the multi-objective design ...
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ژورنال
عنوان ژورنال: Acta Astronautica
سال: 2018
ISSN: 0094-5765
DOI: 10.1016/j.actaastro.2018.05.062