Super-twisting sliding mode control design based on Lyapunov criteria for attitude tracking control and vibration suppression of a flexible spacecraft

The three-axis attitude tracking manoeuvre and vibration suppression of a flexible spacecraft in the presence of external disturbances are investigated in this paper. The spacecraft consists of a rigid hub and two flexible appendages. The Euler–Bernoulli beam theory is used to model the flexible par...

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Bibliographic Details
Main Authors: Reza Nadafi, Mansour Kabganian, Ali Kamali, Mahboobeh Hossein Nejad
Format: Article
Language:English
Published: SAGE Publishing 2019-09-01
Series:Measurement + Control
Online Access:https://doi.org/10.1177/0020294019847696