Attitude Tracking Control for Rigid Spacecraft With Parameter Uncertainties

In this paper, the attitude tracking control problem for rigid spacecraft is investigated in the presence of parameter uncertainties and external disturbances. An extended state observer is designed to estimate the parameter uncertainties and external disturbances. Then, by using the obtained estima...

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Bibliographic Details
Main Authors: Yu-Yao Wu, Ying Zhang, Ai-Guo Wu
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/9000870/