Investigation of the effects of stiffness on control power via a morphing wing technology

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 5, Issue , 2005, Pages 2982-3016

  Vu, Phuc ^a,b   Chavez, Frank ^a,c   Kelkar, Atul ^a,d   Whitmer, Chris ^a,d  

^a IOWA STATE UNIVERSITY   (United States)

^b BOEING COMPANY   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d Iowa State University of Science and Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODELING; CONTROL ENERGY; MECHANICAL ACTUATION SYSTEM; MORPHING WING TECHNOLOGY;

AIRCRAFT; BENDING (DEFORMATION); DEGREES OF FREEDOM (MECHANICS); FLUTTER (AERODYNAMICS); MANEUVERABILITY; OPTIMIZATION; WINGS;

STIFFNESS;

EID: 28844445028     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Raymond L. Bisplinghoff, Holt Ashley, and Robert L. Halfman, Aero elasticity, Dover Publications Inc., Mineola, New York, 1993.
2. Wright-Patterson AFB OH, AFRL's Public Affairs Office, "Active aeroelastic wing technology integrates air vehicle aerodynamics, active controls, and structures to maximize air vehicle performance," public affairs briefs, [online source], URL: http://www.afrlhorizons.com/Briefs/Mar03/ HQ0210.html, [cited 12 April 2003].
3. th AIAA/ISSMO Symposium on multidisciplinary analysis and optimization 4-6 September 2002, Atlanta, Georgia, AIAA 2002-5401.
4. Charbel Farhat, "Flutter in the sky," University of Colorado Boulder, [online report], URL: www.psc.edu/science/farhat.html. [cited 17 April 2003].
5. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit, AIAA-98-2108, 1998.
6. Alexander Bolonkin, Glen Gilyard, "Benefits of variable-geometry wing camber for transport aircraft," NASA/TM-1999, 206586.
7. William A. Lokos, Candila D. Olney, Natalie D. Crawford, Rick Stauf, and Eric Y. Riechenback, "Wing torsional stiffness tests of the active aeroelastic wing F/A-18 airplane," NASA Dry den Flight Research Center, Edwards, California, NASA/TM-2002-210723.
8. Sara Hammond, "Raytheon developing morphing wing structures for cruise missile," media relations, [online report], http://www.raytheon.com, [cited 23 April 2003].
9. Larine Barr, "Wing-warping aircraft makes first flight," Air Force research laboratory public affairs, [online report], http://www.afmc. wpafb.af.mil/HQ-AFMC/PA/index.htm, [cited 15 April 2003].
10. Donald G. Schultz, James L. Melsa, State functions and linear control systems, McGraw-Hill Book Company, 1967.
11. E. L. Houghton, A. E. Brock, Aerodynamics for engineering students, Edward Arnold (publishers) Ltd., London, 1960.
12. Harry L. Trentelman, Anton A. Stoorvogel, Malo Hautus, Control theory for linear systems, Springer-Verlag London Limited 2001.
13. Frank L. Lewis, Vassilis L. Syrmos, Optimal Control, Second Edition, Wiley, John & Sons, Inc., 1995.
14. John J. Bertin, Michael L. Smith, Aerodynamics for engineers, Third Edition, Prentice Hall, Upper Saddle River, New Jersey 1998.
15. Gene F. Franklin, J. David Powell, Abbas Emami-Naeini, Feedback control of dynamic systems, Third Edition, Addison-Wesley Company, 1994.
16. Frank R. Chavez, "Characterizing model variation for robust control of flexible atmospheric flight vehicles," Ph.D. thesis, URL: http://www.enae.umd.edu/pdf/students/PhD/ChavezPhD2000.pdf. 2000 (published), [cited 20 April 03].
17. Bisplinghoff, R. L. and Ashley, H., Principles of aeroelasticity, Dover Publication, 1975.
18. Chris Whitmer, "Modeling and control of a morphing airfoil structure," Master's thesis, Mechanical Engineering Department, Iowa State University, 2003 (published).
19. Brian J. Olson, ME 461, "Mechanical Vibrations, Modal Analysis Lecture Notes," [online class notes], URL: http://www.egr.msu.edu/classes/ me461/olsonbr1/docs/Moda_Analvsis.pdf, [cited 10 November 2002].