Decentralized control of sound radiation using iterative loop recovery.
A decentralized model-based control strategy is designed to reduce low-frequency sound radiation from periodically stiffened panels. While decentralized control systems tend to be scalable, performance can be limited due to modeling error introduced by the unmodeled interaction between neighboring control units. Since bounds on modeling error are not known in advance, it is difficult to ensure the decentralized control system will be robust without making the controller overly conservative. Therefore an iterative approach is suggested, which utilizes frequency-shaped loop recovery. The approach accounts for modeling error introduced by neighboring control loops, requires no communication between subsystems, and is relatively simple. The control strategy is evaluated numerically using a model of a stiffened aluminum panel that is representative of the sidewall of an aircraft. Simulations demonstrate that the iterative approach can achieve significant reductions in radiated sound power from the stiffened panel without destabilizing neighboring control units.
Structural Acoustics Branch, NASA Langley Research Center, Mail Stop 463, Hampton, Virginia 23681, USA. noah.h.schiller@nasa.gov
Noah H
NH
Schiller
Randolph H
RH
Cabell
Chris R
CR
Fuller
D000162:Acoustics / Q000295:instrumentation; D000401:Aircraft; D000535:Aluminum; D003198:Computer Simulation; D004548:Elasticity; D004867:Equipment Design; D005246:Feedback; D016014:Linear Models; D008962:Models, Theoretical; D009038:Motion; D009622:Noise / Q000517:prevention & control; D009716:Numerical Analysis, Computer-Assisted; D013016:Sound; D014159:Transducers; D014732:Vibration
D000535:Aluminum