Tail buffet alleviation of high performance twin tail aircraft using offset piezoceramic stack actuators and acceleration feedback control

[1]  Osama A. Kandil,et al.  FLOW CONTROL AND MODIFICATION FOR ALLEVIATING TWIN-TAIL BUFFET , 1999 .

[2]  Scott M. Murman,et al.  Computation of F/A-18 tail buffet , 1996 .

[3]  Colin H. Hansen,et al.  Control of flexural vibration in stiffened structures using multiple piezoceramic actuators , 1996 .

[4]  C. Liang,et al.  An impedance method for dynamic analysis of active material systems , 1994 .

[5]  Gregory S. Agnes,et al.  Active smart material system for buffet load alleviation , 1995, Smart Structures.

[6]  Chris LaVigna,et al.  Innovative active control of gun barrels using smart materials , 1997, Smart Structures.

[7]  Larry A. Meyn,et al.  Full-scale wind-tunnel studies of F/A-18 tail buffet , 1996 .

[8]  J. Doyle,et al.  Robust and optimal control , 1995, Proceedings of 35th IEEE Conference on Decision and Control.

[9]  Eunsup Sim,et al.  ACTIVE VIBRATION CONTROL OF FLEXIBLE STRUCTURES WITH ACCELERATION FEEDBACK , 1993 .

[10]  Yuan-Cheng Fung,et al.  An introduction to the theory of aeroelasticity , 1955 .

[11]  S. G. Liou,et al.  Flow over a twin-tailed aircraft at angle of attack. II - Temporal characteristics , 1992 .

[12]  Xiaoming Wang,et al.  Electro-mechanical dynamic analysis of the piezoelectric stack , 1996 .

[13]  Pat Barney,et al.  Vibration Control of Stiff Beams and Plates Using Structurally Integrated PZT Stack Actuators , 1997 .

[14]  André Preumont,et al.  Vibration Control of Active Structures: An Introduction , 2018 .

[15]  T. K. Caughey,et al.  On the stability problem caused by finite actuator dynamics in the collocated control of large space structures , 1985 .

[16]  W Moses Robert,et al.  Vertical-tail-buffeting alleviation using piezoelectric actuators: some results of the actively controlled response of buffet-affected tails (ACROBAT) program , 1997, Smart Structures.

[17]  M. Balas.  Active control of flexible systems , 1978 .

[18]  N J Wood,et al.  Experimental investigation of twin-fin buffeting and suppression , 1993 .

[19]  Max F. Platzer,et al.  Effect of leading-edge extension fences on the vortex wake of an F/A-18 model , 1995 .

[20]  Gene F. Franklin,et al.  Feedback Control of Dynamic Systems , 1986 .

[21]  Lewis B. Schiff,et al.  Forebody Tangential Slot Blowing on an Aircraft Geometry , 1994 .

[22]  D. G. Mabey,et al.  Some Aspects of Aircraft Dynamic Loads Due to Flow Separation Meeting (65th) Held in Cesme, Turkey on 4-9 October 1987 , 1988 .

[23]  Osama A. Kandil,et al.  EFFECTIVENESS OF FLOW CONTROL FOR ALLEVIATION OF TWIN-TAIL BUFFET , 1998 .

[24]  D. Brown,et al.  Wind-tunnel studies of F/A-18 tail buffet , 1992 .

[25]  C. J. Goh,et al.  APPROXIMATE POLE PLACEMENT FOR ACCELERATION FEEDBACK CONTROL OF FLEXIBLE STRUCTURES , 1996 .

[26]  C. Liang,et al.  Electromechanical Analysis of Piezoelectric Stack Active Member Power Consumption , 1995 .

[27]  André Preumont,et al.  Active damping by a local force feedback with piezoelectric actuators , 1991 .

[28]  Chris L. Pettit,et al.  Full-scale wind-tunnel pressure measurements of an F/A-18 tail during buffet , 1996 .

[29]  Minh Q. Phan,et al.  Robust controller designs for second-order dynamic systems - A virtual passive approach , 1992 .

[30]  Douglas I. Greenwell,et al.  Vortex control technique for the attenuation of fin buffet , 1993 .

[31]  Randall Hauch,et al.  Reduction of vertical tail buffet response using active control , 1995 .

[32]  Reduction of fluctuations over swept wings using passive and active mini-fences , 1997 .

[33]  W. E. Triplett.  Pressure measurements on twin vertical tails in buffeting flow , 1983 .

[34]  R. Courant,et al.  Methods of Mathematical Physics , 1962 .