Robust autopilot for a flexible missile: loop-shapingH∞ design and real ν-analysis
1998; Wiley; Volume: 8; Issue: 2 Linguagem: Inglês
10.1002/(sici)1099-1239(199802)8
ISSN1099-1239
AutoresJ.P. Friang, Gilles Duc, Jean-Paul Bonnet,
Tópico(s)Stability and Control of Uncertain Systems
ResumoInternational Journal of Robust and Nonlinear ControlVolume 8, Issue 2 p. 129-153 Research Article Robust autopilot for a flexible missile: loop-shaping H∞ design and real ν-analysis Jean-Patrick Friang, Jean-Patrick Friang Aerospatiale—Missiles, 2 à 18 rue Béranger, 92320 Chatillon-sous-Bagneux, France Ecole Supérieure D'Electricité, Service Automatique, Plateau de Moulon, 91192 Gif-sur-Yvette Cedex, FranceSearch for more papers by this authorGilles Duc, Corresponding Author Gilles Duc Ecole Supérieure D'Electricité, Service Automatique, Plateau de Moulon, 91192 Gif-sur-Yvette Cedex, FranceEcole Supérieure D'Electricité, Service Automatique, Plateau de Moulon, 91192 Gif-sur-Yvette Cedex, France===Search for more papers by this authorJean-Paul Bonnet, Jean-Paul Bonnet Aerospatiale—Missiles, 2 à 18 rue Béranger, 92320 Chatillon-sous-Bagneux, FranceSearch for more papers by this author Jean-Patrick Friang, Jean-Patrick Friang Aerospatiale—Missiles, 2 à 18 rue Béranger, 92320 Chatillon-sous-Bagneux, France Ecole Supérieure D'Electricité, Service Automatique, Plateau de Moulon, 91192 Gif-sur-Yvette Cedex, FranceSearch for more papers by this authorGilles Duc, Corresponding Author Gilles Duc Ecole Supérieure D'Electricité, Service Automatique, Plateau de Moulon, 91192 Gif-sur-Yvette Cedex, FranceEcole Supérieure D'Electricité, Service Automatique, Plateau de Moulon, 91192 Gif-sur-Yvette Cedex, France===Search for more papers by this authorJean-Paul Bonnet, Jean-Paul Bonnet Aerospatiale—Missiles, 2 à 18 rue Béranger, 92320 Chatillon-sous-Bagneux, FranceSearch for more papers by this author First published: 04 December 1998 https://doi.org/10.1002/(SICI)1099-1239(199802)8:2 3.0.CO;2-XCitations: 11AboutPDF ToolsRequest permissionExport citationAdd to favoritesTrack citation ShareShare Give accessShare full text accessShare full-text accessPlease review our Terms and Conditions of Use and check box below to share full-text version of article.I have read and accept the Wiley Online Library Terms and Conditions of UseShareable LinkUse the link below to share a full-text version of this article with your friends and colleagues. Learn more.Copy URL Share a linkShare onFacebookTwitterLinked InRedditWechat Abstract This paper considers the control of a bank to turn missile (developed by Aerospatiale) with very lightly damped bending modes. The autopilot is synthesized using the H∞ loop-shaping design procedure of McFarlane and Glover. Robustness against large modelling uncertainties (including parameters and bending modes) is then investigated using the ν-tool, which circumvents the drawback of frequency gridding occurring in μ-analysis. The autopilot of the missile is finally validated on a nonlinear simulator: the performance and the robustness of the design are clearly underlined. © 1998 John Wiley & Sons, Ltd. Citing Literature Volume8, Issue2Special Issue: Robust Control ApplicationsFebruary 1998Pages 129-153 RelatedInformation
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