MODEL PREDICTIVE CONTROL FOR VERY FLEXIBLE AIRCRAFT BASED ON LINEAR PARAMETER VARYING REDUCED-ORDER MODELS (Englisch)
- Neue Suche nach: Pereira, M.
- Neue Suche nach: Duan, M.
- Neue Suche nach: Cesnik, C.
- Neue Suche nach: Kolmanovsky, I.
- Neue Suche nach: Vetrano, F.
- Neue Suche nach: Pereira, M.
- Neue Suche nach: Duan, M.
- Neue Suche nach: Cesnik, C.
- Neue Suche nach: Kolmanovsky, I.
- Neue Suche nach: Vetrano, F.
In:
19th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2022) ; Volume 2 of 4
; 881-898
;
2023
- Aufsatz (Konferenz) / Print
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Titel:MODEL PREDICTIVE CONTROL FOR VERY FLEXIBLE AIRCRAFT BASED ON LINEAR PARAMETER VARYING REDUCED-ORDER MODELS
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Beteiligte:Pereira, M. ( Autor:in ) / Duan, M. ( Autor:in ) / Cesnik, C. ( Autor:in ) / Kolmanovsky, I. ( Autor:in ) / Vetrano, F. ( Autor:in )
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Kongress:International Forum on Aeroelasticity and Structural Dynamics ; 19. ; 2022 ; Madrid
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Erschienen in:
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Verlag:
- Neue Suche nach: Curran Associates, Inc.
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Erscheinungsort:Red Hook, NY
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Erscheinungsdatum:2023
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Datenquelle:
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
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EXPERIMENTAL VALIDATION OF MODEL PREDICTIVE CONTROLLERS FOR LOAD ALLEVIATION IN VERY FLEXIBLE AIRCRAFTPereira, M. / Chaves, G. / Bertolin, R. / Kolmanovsky, I. / Cesnik, C. et al. | 2023
- 679
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ACTIVE FLUTTER SUPPRESSION FROM AN INDUSTRIAL PERSPECTIVEFischer, A. / Schroder, F. / Thormann, R. et al. | 2023
- 698
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WING-TAILPLANE FLOW INTERACTION: FLIGHT TEST DATA ANALYSIS FROM STALL FLIGHTSKoopmans, W. / Klabes, A. / Gojny, M. et al. | 2023
- 708
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ESTIMATION OF GLOBAL STRUCTURAL AIRCRAFT LOADS DUE TO ATMOSPHERIC DISTURBANCES FOR STRUCTURAL FATIGUE ESTIMATIONSchulz, S. / Ossmann, D. et al. | 2023
- 723
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FLEXIBLE-WING DESIGN PROCESS FOR TU-FLEX DEMONSTRATORGonzalez, P. / Shahi, H. / Meddaikar, Y. / Kruger, W. / Silvestre, F. et al. | 2023
- 742
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ACTIVE FLUTTER SUPPRESSION OF A TWO-DIMENSIONAL AIRFOIL WITH ACTUATOR SATURATIONMicheli, B. et al. | 2023
- 762
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REAL TIME FLUTTER ANALYSIS IN AIRBUS DEFENCE AND SPACEHerrero, F. / Torralbo, P. / Isidoro, E. / Nogales, M. et al. | 2023
- 781
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GROUND LOADS DYNAMIC ANALYSIS OF AN AIRCRAFT WITH A MAGNETORHEOLOGICAL SHOCK ABSORBER INSTALLEDContreras, A. / Martinez, J. / Vinas, E. / Dominguez, M. / Diaz, E. et al. | 2023
- 797
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GUST LOAD ALLEVIATION OF A TWO DIMENSIONAL NONLINEAR WING USING NONLINEAR ENERGY SINKSAmoozgar, M. / Garvey, S. / Friswell, M. / Cooper, J. / Ajaj, R. et al. | 2023
- 810
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DYNAMIC LANDING ASSESSMENT FOR A LONG ENDURANCE UAV - CONTRIBUTION OF STRUCTURAL FLEXIBILITY AND OF UNSTEADY AERODYNAMICSMastromauro, P. / Fleischer, D. et al. | 2023
- 825
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AEROELASTIC AND GUST REJECTION CHARACTERISTICS OF A SLENDER WING SUSPENDED BY A VISCOELASTIC CORDJayatilake, S. / Lowenberg, M. / Woods, B. / Titurus, B. et al. | 2023
- 844
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ANALYSIS OF RIDE QUALITIES IN TRANSONIC HIGH-ASPECT-RATIO-WING AIRCRAFTSanghi, D. / Riso, C. / Cesnik, C. / Vetrano, F. et al. | 2023
- 861
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REDUCED ORDER SOLVER FOR GENERAL AEROELASTIC PROBLEMSTorregrosa, A. / Garcia-Tiscar, J. / Quintero, P. / Cremades, A. et al. | 2023
- 881
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MODEL PREDICTIVE CONTROL FOR VERY FLEXIBLE AIRCRAFT BASED ON LINEAR PARAMETER VARYING REDUCED-ORDER MODELSPereira, M. / Duan, M. / Cesnik, C. / Kolmanovsky, I. / Vetrano, F. et al. | 2023
- 899
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LOAD ALLEVIATION USING SPANWISE MORPHING TRAILING EDGE CONCEPTPilakkadan, J. / Ajaj, R. / Amoozgar, M. et al. | 2023
- 919
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SAFE WIND TUNNEL FLUTTER TEST USING A SHAKER AND MASS MARGINSKarpel, M. / McCrink, M. / Heidersbach, R. / Seth, D. et al. | 2023
- 933
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APPLICATION OF SPARSE IDENTIFICATION TO THE NON-LINEAR PANEL FLUTTER PROBLEMGambioli, F. / Mastroddi, F. / Fasel, U. / Kutz, N. / Brunton, S. et al. | 2023
- 945
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AEROELASTIC WAVE PROPAGATIONS OF METAMATERIAL UAV WINGMurugan, S. / Sunny et al. | 2023
- 957
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HIGH-FIDELITY AEROSTRUCTURAL OPTIMIZATION WITH A GEOMETRICALLY NONLINEAR FLUTTER CONSTRAINTGray, A. / Riso, C. / Jonsson, E. / Martins, J. / Cesnik, C. et al. | 2023
- 978
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GUST AND MANOUVRE LOADS ALLEVIATION TECHNOLOGIES: OVERVIEW, RESULTS AND LESSON LEARNED IN THE FRAMEWORK OF THE CS2 AIRGREEN2 PROJECTToffol, F. / Marchetti, L. / Ricci, S. / Fonte, F. / Capello, E. / Malisani, S. et al. | 2023
- 1002
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ACTIVE FLUTTER SUPPRESSION OF A HIGHLY FLEXIBLE SWEPT WING THROUGH MULTIPLE FLAP CONTROLWaitz, S. et al. | 2023
- 1016
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POST-FLUTTER DYNAMICS OF THE PAZY WING GEOMETRICALLY NONLINEAR BENCHMARK MODELRiso, C. / Cesnik, C. et al. | 2023
- 1034
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DEVELOPMENT OF AN ACTIVE AEROELASTIC PARAMETRIC WING APPARATUSSchildkamp, R. / Wang, X. / Chang, J. / Breuker, R. De / Sodja, J. et al. | 2023
- 1053
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INCREMENTAL NONLINEAR CONTROL FOR AEROELASTIC WING LOAD ALLEVIATION AND FLUTTER SUPPRESSIONSchildkamp, R. / Chang, J. / Sodja, J. / Breuker, R. De / Wang, X. et al. | 2023
- 1068
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FLUTTER ANALYSIS OF THE BENCHMARK SUPERCRITICAL WING IN THE PRESENCE OF SHOCK BUFFETPoplingher, L. / Raveh, D. et al. | 2023
- 1093
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3D-PRINTED SWEPT-WING WIND TUNNEL MODEL CHARACTERIZATION FOR AEROELASTIC STUDIESSharqi, B. / Cesnik, C. / Joels, T. / Raveh, D. et al. | 2023
- 1114
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EXPERIMENTAL STUDIES ON DYNAMIC FREEPLAY NONLINEARITYFonzi, N. / Curasi, H. / Ricci, S. / Livne, E. et al. | 2023
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STATE-SPACE AEROELASTIC MODELLING OF FLYING WINGSAng, E. / Ng, B. et al. | 2023
- 1145
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TAXI VIBRATION TESTING APPLICATION IN SKYDWELLER AEROCarre, A. del / Sarabia, E. / Moreno, R. et al. | 2023
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EMBEDDED FLIGHT VIBRATION TESTING SYSTEMFOR ONLINE FLUTTER MONITORING OF UAVSSoal, K. / Thiem, C. / Meier, T. / Volkmar, R. / Sinske, J. / Govers, Y. / Boswald, M. et al. | 2023
- 1169
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COMPUTATION OF LIMIT CYCLE OSCILLATIONS AND THEIR STABILITIES IN NONLINEAR AEROELASTIC SYSTEMS USING HARMONIC BALANCE METHODSMcGurk, M. / Yuan, J. et al. | 2023
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A CONTROL DESIGN FRAMEWORK FOR GUST LOAD ALLEVIATION IN MORE FLEXIBLE AIRCRAFTDussler, S. / Palacios, R. et al. | 2023
- 1211
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RELIABILITY AND REPRESENTATIVENESS OF COLLECTED USAGE DATA FOR JUSTIFICATION OF FATIGUE DESIGN ASSUMPTIONSPostels, M. / Gojny, M. et al. | 2023
- 1220
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A COMPARISON OF DIRECT AND SAMPLING-BASED FLUTTER SOLUTION METHODS USING CFDSimiriotis, N. / Palacios, R. et al. | 2023
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DEVELOPMENT OF AN AEROELASTIC STABILITY MODULE FOR WING PLANFORM OPTIMIZATIONTorrigiani, F. / Nagel, B. / Cavallaro, R. et al. | 2023
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AN INTEGRATED FLEXIBLE AIRCRAFT MODEL FOR OPTIMAL CONTROL SURFACE SCHEDULING OF MANOEUVRE LOAD ALLEVIATION AND WING SHAPE CONTROL FUNCTIONSKier, T. et al. | 2023
- 1273
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COMBINED TAXI AND GROUND VIBRATION TESTING TO SPEED UP THE AEROELASTIC CLEARANCE FOR FIRST FLIGHTSilva, D. da et al. | 2023
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C295 GROUND VIBRATION TESTING: ASSESSMENT OF BOUNDARY CONDITIONSCasillas, T. / Diego, R. de / Jimenez, H. / Nicolas, F. de et al. | 2023