Tekin, Raziye und Pfifer, Harald (2013) Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L2-norm Framework. In: Selected Papers of the Second CEAS Specialist Conference on Guidance, Navigation and Control, Seiten 3-14. Springer Verlag. 2nd CEAS Specialist Conference on Guidance, Navigation & Control, 2013-04-10 - 2013-04-12, Delft, The Netherlands. doi: 10.1007/978-3-642-38253-6_1. ISBN 978 3 642 38252 9.
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Offizielle URL: http://link.springer.com/chapter/10.1007/978-3-642-38253-6_1
Kurzfassung
This paper deals with the application of a linear parameter varying (LPV) controller synthesis for a modern air defense missile model. The model represents a challenging control problem due to the wide operation range. First, an LPV model of the missile is constructed via a novel approach of function substitution. Then, an LPV controller is designed based on the induced L2-norm framework. A mixed sensitivity weighting scheme is applied to specify the performance requirements. In order to fulfill various time and frequency domain criteria, a multiobjective optimization is used to tune the weighting functions of the mixed sensitivity weighting scheme. Finally, the robustness and performance of the controller is evaluated by nonlinear simulations.
elib-URL des Eintrags: | https://elib.dlr.de/83742/ | ||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||
Titel: | Linear Parameter Varying Control of an Agile Missile Model Based on the Induced L2-norm Framework | ||||||||||||||||||||||||||||
Autoren: |
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Datum: | April 2013 | ||||||||||||||||||||||||||||
Erschienen in: | Selected Papers of the Second CEAS Specialist Conference on Guidance, Navigation and Control | ||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||
DOI: | 10.1007/978-3-642-38253-6_1 | ||||||||||||||||||||||||||||
Seitenbereich: | Seiten 3-14 | ||||||||||||||||||||||||||||
Herausgeber: |
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Verlag: | Springer Verlag | ||||||||||||||||||||||||||||
Name der Reihe: | Advances in Aerospace Guidance, Navigation and Control | ||||||||||||||||||||||||||||
ISBN: | 978 3 642 38252 9 | ||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||
Stichwörter: | LPV, Missile control, Robust control, nonlinear control, gain scheduling, flight control | ||||||||||||||||||||||||||||
Veranstaltungstitel: | 2nd CEAS Specialist Conference on Guidance, Navigation & Control | ||||||||||||||||||||||||||||
Veranstaltungsort: | Delft, The Netherlands | ||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 10 April 2013 | ||||||||||||||||||||||||||||
Veranstaltungsende: | 12 April 2013 | ||||||||||||||||||||||||||||
Veranstalter : | TU-Delft | ||||||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||||||
HGF - Programm: | Luftfahrt | ||||||||||||||||||||||||||||
HGF - Programmthema: | Starrflügler (alt) | ||||||||||||||||||||||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||||||||||
DLR - Forschungsgebiet: | L AR - Starrflüglerforschung | ||||||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Systeme & Kabine (alt) | ||||||||||||||||||||||||||||
Standort: | Oberpfaffenhofen | ||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Systemdynamik und Regelungstechnik > Flugzeug-Systemdynamik | ||||||||||||||||||||||||||||
Hinterlegt von: | Looye, Dr. Gertjan | ||||||||||||||||||||||||||||
Hinterlegt am: | 02 Sep 2013 11:57 | ||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:50 |
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