Adaptive sliding mode attitude tracking control for flexible spacecraft systems based on the Takagi-Sugeno fuzzy modelling method

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Bibliographic Details
Published in:Acta Astronautica Vol. 175; pp. 570 - 581
Main Authors: Ang Li, Ming Liu, Yan Shi
Format: Journal Article
Language:Japanese
Published: Elsevier BV 01.10.2020
ISSN:0094-5765
Online Access:Get full text
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Description
ISSN:0094-5765
DOI:10.1016/j.actaastro.2020.05.041