Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement
type: Item
instance of: scholarly article
title: Finite-time sliding mode attitude control for rigid spacecraft without angular velocity measurement
zbMATH Open document ID: 1367.93130
author: Shikai Shao
author: Qun Zong
author: Bailing Tian
author: Fang Wang
published in: Journal of the Franklin Institute
publication date: 2017-07-27T00:00:00Z
Mathematics Subject Classification ID: 93B12
Mathematics Subject Classification ID: 93C40
Mathematics Subject Classification ID: 93B07
Mathematics Subject Classification ID: 70P05
Mathematics Subject Classification ID: 93B40
zbMATH DE Number: 6754211
zbMATH Keywords: finite-time sliding mode attitude control
zbMATH Keywords: rigid spacecraft
zbMATH Keywords: adaptive update law
zbMATH Keywords: angular velocity calculation algorithm (AVCA)
MaRDI profile type: Publication
full work available at URL: j.jfranklin.2017.04.020
OpenAlex ID: W2613336238
cites work: Q3596154
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cites work: Attitude stabilization of rigid spacecraft with finite-time convergence
cites work: Adaptive attitude tracking control for rigid spacecraft with finite-time convergence
cites work: Finite‐time attitude control of multiple rigid spacecraft using terminal sliding mode
cites work: Passivity-based adaptive attitude control of a rigid spacecraft
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cites work: A globally convergent angular velocity observer for rigid body motion
cites work: Distributed finite-time velocity-free attitude coordination control for spacecraft formations
cites work: Distributed adaptive containment control for second-order multi-agent systems via NTSM
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cites work: Distributed containment control for Lagrangian networks with parametric uncertainties under a directed graph
DOI: 10.1016/J.JFRANKLIN.2017.04.020
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description: scientific article; zbMATH DE number 6754211