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1. 2. 3. 4. 5. 6. 7. © Vibration Suppression In Rotating Beams Using Active Modal Control Khulief, YA ACADEMIC PRESS LTD, JOURNAL OF SOUND AND VIBRATION;

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Presentation on theme: "1. 2. 3. 4. 5. 6. 7. © Vibration Suppression In Rotating Beams Using Active Modal Control Khulief, YA ACADEMIC PRESS LTD, JOURNAL OF SOUND AND VIBRATION;"— Presentation transcript:

1 1. 2. 3. 4. 5. 6. 7. © Vibration Suppression In Rotating Beams Using Active Modal Control Khulief, YA ACADEMIC PRESS LTD, JOURNAL OF SOUND AND VIBRATION; pp: 681-699; Vol: 242 King Fahd University of Petroleum & Minerals http://www.kfupm.edu.sa Summary Advances in technology and the underlying demand for achieving high performance has resulted in a class of light-weight high-speed mechanical systems. Light-weight mechanical components are prone to appreciable elastic deformations and experience vibrational motions. Vibration suppression in rotating elastic members is of major importance in many engineering applications. Examples are robot manipulators, propellers, turbomachines, high-speed flexible mechanisms, and space deployable systems. Active control falls among the most feasible techniques for vibration suppression in rotating structures, where passive techniques may become ineffective or impractical. The vibrational motion of the rotating elastic member is represented by a finite element dynamic model, which is written in terms of a reduced set of modal co-ordinates. A realistic set of modal co-ordinates that accounts for the dynamically induced stiffening effect due to reference rotation is introduced. Pointwise observation and control art: employed in association with an optimal state-variable feedback strategy. The control scheme developed is applied to a rotating beam, and the dynamic responses of both the controlled and residual frequency subsystems are numerically evaluated. (C) 2001 Academic Press. References: ANKARALI A, 1997, J SOUND VIB, V204, P162 BAILEY T, 1985, J GUID CONTROL DYNAM, V8, P605 BALAS MJ, 1978, IEEE T AUTOMAT CONTR, V23, P673 BALAS MJ, 1978, SIAM J CONTROL OPTIM, V16, P450 BERNNAN MJ, 1998, AM SOC MECH ENG J VI, V120, P1 BERNZEN W, 1999, J INTELL ROBOT SYST, V24, P69 BLOCK JF, 1988, AM I AERONAUTICS AST, V21, P838 Copyright: King Fahd University of Petroleum & Minerals; http://www.kfupm.edu.sa

2 8. 9. 10. 11. 12. 13. 14. 15. 16. 17. 18. 19. 20. 21. 22. 23. 24. 25. 26. 27. 28. 29. 30. 31. 32. 33. 34. 35. 36. 37. © BURDISSO RA, 1998, J SOUND VIB, V214, P817 CLARK RL, 1992, J ACOUST SOC AM, V92, P871 COTTERELL M, 1975, STRESS VIBRATION NOI, P253 CROSBY MJ, 1973, SHOCK VIB B, V43, P119 DUKE S, 1988, AUTOMATICA, V24, P619 FULLER CR, 1990, INT C REC DEV AIR ST, P657 FUNG RF, 1998, J SOUND VIB, V214, P605 IWENS R, 1980, JOINT AUT CONTR C SA KHULIEF YA, 1980, THESIS U HERTFORDSHI KHULIEF YA, 1989, ASME J DYNAMIC SYSTE, V111, P521 KHULIEF YA, 1989, J SOUND VIB, V134, P87 KHULIEF YA, 1992, COMPUT METHOD APPL M, V97, P23 KHULIEF YA, 1997, FINITE ELEM ANAL DES, V26, P41 KWAKERNAAK H, 1972, LINEAR OPTIMAL CONTR LAZAN BJ, 1968, DAMPING MAT MEMBERS LIKENS P, 1972, AM I AERONAUTICS AST, V11, P1251 LIKINS PW, 1967, AIAA J, V5, P1304 MARSH ER, 1998, J VIB ACOUST, V120, P188 MEIROVITCH L, 1974, AIAA J, V12, P1337 MEIROVITCH L, 1980, J GUIDANCE CONTROL, V3, P569 NELSON PA, 1992, ACTIVE CONTROL SOUND SETOLA R, 1998, J SOUND VIB, V213, P777 SHABANA AA, 1983, ASME, V105, P370 SILJAK DD, 1976, AUTOMATICA, V12, P309 SKIDMORE GR, 1985, J SOUND VIB, V101, P149 SPANOS TJ, 1991, J GUIDANCE, V14, P260 STANWAY R, 1981, ASME, V103, P383 STURLA FA, 1996, J VIB ACOUST, V118, P463 WALKER L, 1976, J SOUND VIBRATIONS, V46, P157 YANG SM, 1999, J APPL MECH-T ASME, V66, P254 For pre-prints please write to: abstracts@kfupm.edu.sa Copyright: King Fahd University of Petroleum & Minerals; http://www.kfupm.edu.sa


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