Nonlinear dynamics and control of integrally actuated helicopter blades

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

Volumn 9, Issue , 2005, Pages 5847-5861

  Traugott, Johannes P ^a,c   Patil, Mayuresh J ^b,d   Holzapfel, Florian ^a,c  

^a TECHNICAL UNIVERSITY OF MUNICH   (Germany)

^b Virginia Polytechnic Institute and State University   (United States)

^c Institute of Flight Mechanics and Flight Control   (Germany)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DAMPING; FINITE ELEMENT METHOD; HELICOPTERS; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS;

HELICOPTER BLADES; INTRINSIC KINEMATICAL EQUATIONS; SENSOR MODELS;

TURBOMACHINE BLADES;

EID: 28844468531     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-2271     Document Type: Conference Paper

References (10)

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2. th American Helicopter Society Annual Forum, Phoenix, Arizona, May 2003.
3. Volovoi, V. V., Hodges, D. H., Cesnik, C. E. S., and Popescu, B., "Assessment of beam modeling methods for rotor blade applications," Mathematical and Computer Modelling, Vol. 33, No. 10-11, May - June 2001, pp. 1099-1112.
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8. Hodges, D. H. and Rutkowski, M. J., "Free-Vibration Analysis of Rotating Beams by a Variable-Order Finite-Element Method," AIAA Journal, Vol. 19, No. 11, 1981, pp. 1459-1466.
9. Cesnik, C., Shin, S., and Wilbur, M., "Dynamic Response of Active Twist Rotor Blades," Smart Materials and Structures, Vol. 10, 2001, pp. 62-76.
10. Preumont, A., Vibration Control of Active Structures - An Introduction, G.M.L. Gladwell, Waterloo, Ontario, Candada, 2001.