Vibration attenuation of a flexible beam mounted on a rotating compliant hub

被引:4
作者
El-Sinawi, AH [1 ]
机构
[1] King Fahd Univ Petr & Minerals, Dept Mech Engn, Dhahran 31261, Saudi Arabia
关键词
base excitation; optimal control; LQG; estimation; rotating machinery;
D O I
10.1243/095965104322892285
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
This study considers the problem of attenuating the vibration of a slender flexible beam mounted on a compliant rotating hub without the need for sensor(s) placement at the beam. A modal state-space model of the beam-hub system dynamics is constructed from the first ten modes of vibration of the system. A reduced-order optimal observer is utilized to estimate the deflection of the beam tip from measurements of the horizontal and vertical deflections of the hub. Two orthogonal actuators are used to manipulate the hub such that the relative motion between the hub and the tip of the beam is minimized. Hence, the demand on the control effort is to force the beam tip and the hub to vibrate as a rigid body. The horizontal control effort is a function of the difference between the measured horizontal hub deflection and the estimated horizontal tip deflection, and the same is true for the vertical control effort. Simulation of the proposed control strategy is carried out and the results are presented.
引用
收藏
页码:121 / 135
页数:15
相关论文
共 17 条
  • [1] Al-Bedoor B. O., 2002, Shock and Vibration Digest, V34, P455
  • [2] FREQUENCY-RESPONSE OF NONPROPORTIONALLY DAMPED, LUMPED PARAMETER, LINEAR DYNAMIC-SYSTEMS
    BELLOS, J
    INMAN, DJ
    [J]. JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 1990, 112 (02): : 194 - 201
  • [3] An LQ approach to active control of vibrations in helicopters
    Bittanti, S
    Lorito, F
    Strada, S
    [J]. JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 1996, 118 (03): : 482 - 488
  • [4] Optimal vibration estimation of a non-linear flexible beam mounted on a rotating compliant hub
    El-Sinawi, A
    Hamdan, MN
    [J]. JOURNAL OF SOUND AND VIBRATION, 2003, 259 (04) : 857 - 872
  • [5] Active isolation using a Kalman estimator-based controller
    El-Sinawi, A
    Kashani, R
    [J]. JOURNAL OF VIBRATION AND CONTROL, 2001, 7 (08) : 1163 - 1173
  • [6] MODEL-REDUCTION FOR FLEXIBLE SPACE STRUCTURES
    GAWRONSKI, W
    WILLIAMS, T
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1991, 14 (01) : 68 - 76
  • [7] Gawronski W., 1998, DYNAMICS CONTROL STR
  • [8] Non-linear dynamics and control of chaos for a tachometer
    Ge, ZM
    Shiue, JS
    [J]. JOURNAL OF SOUND AND VIBRATION, 2002, 253 (04) : 773 - 793
  • [9] Griffin JerryH., 1990, INT J TURBO JET ENG, V7, P297, DOI DOI 10.1515/TJJ.1990.7.3-4.297
  • [10] Stabilization of motion of helicopter rotor blades using delayed feedback - Modelling, computer simulation and experimental verification
    Krodkiewski, JM
    Faragher, JS
    [J]. JOURNAL OF SOUND AND VIBRATION, 2000, 234 (04) : 591 - 610