Comparison of structural-acoustic control designs on an active composite panel

Journal of Sound and Vibration

Volumn 244, Issue 5, 2001, Pages 761-778

  Bingham, B ^a   Atalla, M J ^a   Hagood, N W ^a  

^a Massachusetts Institute of Technology Cambridge   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON FIBERS; FEEDBACK CONTROL; LEAST SQUARES APPROXIMATIONS; STRUCTURAL PANELS; VIBRATIONS (MECHANICAL);

LINEAR QUADRATIC GAUSSIAN; OPTIMAL FEEDBACK; RATE FEEDBACK; STRUCTURAL ACOUSTIC CONTROL;

ACOUSTIC VARIABLES CONTROL;

EID: 0035954625     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.2000.3536     Document Type: Article

References (33)

1. The minimum power output of a pair of free field monopoles
2. A multiple error LMS algorithm and its application to the active control of sound and vibration
3. Active control of sound radiation from a vibrating rectangular panel by sound sources and vibration inputs: An experimental comparison
4. Control of sound radiation with active/adaptive structures
5. Active control of sound radiation from cylinders with piezoelectric actuators and structural-acoustic sensing
6. Causality analysis of feedforward-controlled systems with broadband input
7. Control of sound radiation with adaptive structures
8. Active control of broadband structural vibration using the LMS adaptive algorithm
9. Test-bed design and modelling for aircraft interior acoustic control
10. Structural-acoustic design and control of an integrally actuated composite panel
11. Active structural acoustic control of broadband disturbances
12. Radiation resistance of a rectangular panel
13. A sub-space algorithm for identification of discrete time frequency domain power spectra
14. State space feedback control of sound radiation using structural sensors and structural control inputs
15. Hover testing of a 1/6th Mach scale CH-47D blade with integral twist actuation
16. Broadband active structural-acoustic control of a fuselage test-bed using collocated piezoelectric sensors and actuators
17. Reconfigurable arrays for broadband feedback control of aircraft fuselage vibrations
18. Reconfigurable arrays of collocated sensors and actuators for modal isolation
19. Active structural-acoustic control of a think-walled cylindrical shell
20. Piezoelectric fiber composites with interdigitated electrodes
21. Neo-classical control of structures
22. On-line system identification and control design for flexible structures
23. A multiple error lms algorithm and its application to the active control of sound and vibration
24. Active control of broadband structural vibration using the LMS adaptive algorithm
25. Control of broadband acoustic radiation with adaptive structures
26. Experiments on active control of structurally radiated sound using multiple piezoceramic actuators