Nonlinear \(H_\infty\) robust control applied to F-16 aircraft with mass uncertainty using control surface inverse algorithm
type: Item
instance of: scholarly article
title: Nonlinear \(H_\infty\) robust control applied to F-16 aircraft with mass uncertainty using control surface inverse algorithm
zbMATH Open document ID: 1201.93037
author: Chien-Chun Kung
published in: Journal of the Franklin Institute
publication date: 2010-11-05T00:00:00Z
Mathematics Subject Classification ID: 93B36
Mathematics Subject Classification ID: 93C95
Mathematics Subject Classification ID: 93C10
Mathematics Subject Classification ID: 93B52
zbMATH DE Number: 5810736
zbMATH Keywords: nonlinear \(H_\infty\) control
zbMATH Keywords: control surface inverse algorithm
zbMATH Keywords: robust
zbMATH Keywords: prefilter
MaRDI profile type: Publication
full work available at URL: j.jfranklin.2008.05.002
OpenAlex ID: W1993607586
cites work: Flight control design using non-linear inverse dynamics
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cites work: Spacecraft Euler parameter tracking of large-angle maneuvers via sliding mode control
cites work: Disturbance attenuation and H/sub infinity /-control via measurement feedback in nonlinear systems
cites work: L/sub 2/-gain analysis of nonlinear systems and nonlinear state-feedback H/sub infinity / control
DOI: 10.1016/J.JFRANKLIN.2008.05.002
description: scientific article; zbMATH DE number 5810736