Active vibration control of nonlinear flexible structures via reduction on spectral submanifolds
arXiv:2408.07252 · doi:10.1007/s11071-024-10801-w
Abstract
Large amplitude vibrations can cause hazards and failure to engineering structures. Active control has been an effective strategy to suppress vibrations, but it faces great challenges in the real-time control of nonlinear flexible structures. Here, we present a control design framework using reductions on aperiodic spectral submanifolds (SSMs) to address the challenges. We formulate high-dimensional nonlinear optimal control problems to suppress the vibrations and then use the SSM-based reductions to transform the original optimal control problems into low-dimensional linear optimal control problems. We further establish extended linear quadratic regulators to solve the reduced optimal control problems, paving the road for real-time active control of nonlinear flexible structures. We demonstrate the effectiveness of our control design framework via a suite of examples with increasing complexity, including a finite element model of an aircraft wing with more than 130,000 degrees of freedom.
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