Fault-tolerant sliding mode attitude tracking control for flexible spacecraft with disturbance and modeling uncertainty

This article investigates the attitude tracking control problem for a class of flexible spacecraft with a redundant four reaction wheels’ setting. In this study, inertia uncertainties, external disturbance, wheel torque saturation, and configuration misalignment are taken into account simultaneously...

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Bibliographic Details
Main Authors: Xibin Cao, Chengfei Yue, Ming Liu
Format: Article
Language:English
Published: SAGE Publishing 2017-03-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814017690341