Boundary control of flexible aircraft wings for vibration suppression

DOI10.1080/00207179.2018.1442025zbMath1425.93131OpenAlexW2792708828MaRDI QIDQ5240697

Xiuyu He, Yao Yu, Yunan Chen, Wei He, Xinxing Mu, Chang-Yin Sun

Publication date: 29 October 2019

Published in: International Journal of Control (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/00207179.2018.1442025

zbMATH Keywords

boundary controlpartial differential equationdistributed parameter systemflexible structureflexible aircraft wings

Mathematics Subject Classification ID

Control/observation systems governed by partial differential equations (93C20) Application models in control theory (93C95) Random vibrations in mechanics of particles and systems (70L05)

Related Items (2)

Nonlinear uncertain systems with nonlinear control channel and unilateral input constraints ⋮ Boundary control of a vertical nonlinear flexible manipulator considering disturbance observer and deflection constraint with torque and boundary force feedback signals

Cites Work

• Nonlinear stabilization through wave PDE dynamics with a moving uncontrolled boundary
• Adaptive boundary control of store induced oscillations in a flexible aircraft wing
• Static output feedback control via PDE boundary and ODE measurements in linear cascaded ODE-beam systems
• Modeling and vibration control of a flexible aerial refueling hose with variable lengths and input constraint
• Optimal boundary control with critical penalization for a PDE model of fluid-solid interactions
• The active disturbance rejection and sliding mode control approach to the stabilization of the Euler-Bernoulli beam equation with boundary input disturbance
• Boundary Control of PDEs
• Arbitrary Decay Rate for Euler-Bernoulli Beam by Backstepping Boundary Feedback

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