TY - GEN
T1 - CONTROL OF BENDING AND TWISTING VIBRATION IN NON-ISOTHERMAL BEAMS
AU - Wetherhold, Robert C.
AU - Aldraihem, Osama J.
N1 - Publisher Copyright:
© 1996 American Society of Mechanical Engineers (ASME). All rights reserved.
PY - 1996
Y1 - 1996
N2 - Vibration control of a beam which experiences a slowly changing through-thickness temperature variation is considered. This temperature variation produces thermal moments and curvatures which are assumed to change slowly with respect to the vibration frequencies. By proposing a Lyapunov controller which relies on a definition of strain energy without thermal expansion terms, stability of vibration control and removal of thermal curvatures are assured. By proposing a Lyapunov controller based on strain energy including thermal expansion terms, stability is assured but the thermal curvatures remain. The effect of temperature on the sensor output is included. A laminated beam with full sensor (all mode) coverage is used to illustrate the method. The continuous system is simulated using a discretized (finite element) approximation, and the successful operation of both controllers is demonstrated. The effects of the host beam stiffness and the ratio of actuator thickness to host beam thickness are determined.
AB - Vibration control of a beam which experiences a slowly changing through-thickness temperature variation is considered. This temperature variation produces thermal moments and curvatures which are assumed to change slowly with respect to the vibration frequencies. By proposing a Lyapunov controller which relies on a definition of strain energy without thermal expansion terms, stability of vibration control and removal of thermal curvatures are assured. By proposing a Lyapunov controller based on strain energy including thermal expansion terms, stability is assured but the thermal curvatures remain. The effect of temperature on the sensor output is included. A laminated beam with full sensor (all mode) coverage is used to illustrate the method. The continuous system is simulated using a discretized (finite element) approximation, and the successful operation of both controllers is demonstrated. The effects of the host beam stiffness and the ratio of actuator thickness to host beam thickness are determined.
UR - https://www.scopus.com/pages/publications/85169163109
U2 - 10.1115/IMECE1996-0654
DO - 10.1115/IMECE1996-0654
M3 - Conference contribution
AN - SCOPUS:85169163109
T3 - ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)
SP - 445
EP - 453
BT - Aerospace
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 1996 International Mechanical Engineering Congress and Exposition, IMECE 1996
Y2 - 17 November 1996 through 22 November 1996
ER -