Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft
type: Item
instance of: scholarly article
title: Robust output feedback attitude tracking control for rigid-flexible coupling spacecraft
zbMATH Open document ID: 1404.93028
author: Y. Aharonov
published in: Journal of the Franklin Institute
publication date: 2018-12-18T00:00:00Z
Mathematics Subject Classification ID: 93D20
Mathematics Subject Classification ID: 93B52
Mathematics Subject Classification ID: 93B35
Mathematics Subject Classification ID: 93C95
zbMATH DE Number: 6994698
zbMATH Keywords: robust attitude tracking control
zbMATH Keywords: feedback attitude tracking control
zbMATH Keywords: rigid-flexible coupling spacecraft
zbMATH Keywords: asymptotic stability
MaRDI profile type: Publication
full work available at URL: j.jfranklin.2017.02.031
OpenAlex ID: W2592756796
cites work: T-S fuzzy-model-based piecewise \(\mathcal{H}_\infty\) output feedback controller design for networked nonlinear systems with medium access constraint
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cites work: New results on H∞ dynamic output feedback control for Markovian jump systems with time-varying delay and defective mode information
cites work: Mode-dependent nonrational output feedback control for continuous-time semi-Markovian jump systems with time-varying delay
DOI: 10.1016/J.JFRANKLIN.2017.02.031
description: scientific article; zbMATH DE number 6994698