Parametric FEM-Based Analysis on Adaptive Vein Morphology of Dragonfly Wings Toward Material Efficiency. [PDF]
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The overlap of anti-Black and anti-protest rhetoric: How far-right political commentators preserve anti-Black racist stereotypes in the context of Black Lives Matter debates. [PDF]
Hunt A, Demasi M, Goodman S.
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Dimensions of Social Capital for Supporting Informal Carers of Patients With Advanced Chronic Illness in the Community: A Concept Mapping Study. [PDF]
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Signatures of Motion: Decomposition of Adaptive Morphing Flight in Harris’ Hawks
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Trajectory Tracking Control for a Three-Dimensional Flexible Wing
IEEE Transactions on Control Systems Technology, 2022This brief mainly considers trajectory tracking and vibration suppression for a 3-D flexible wing. The dynamical model of the flexible wing is regarded as a distributed parameter system, which is described by partial differential equations and ordinary ...
Wei He +3 more
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Adaptive Internal Model Control for a Flexible Wing With Unsteady Aerodynamic Loads
IEEE Transactions on Cybernetics, 2023This article proposes adaptive internal model controls for the collocated output regulation of a flexible wing, where distributed disturbances, boundary disturbances, and references are from an exactly unknown exosystem.
Tingting Meng +3 more
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Robust output regulation for a flexible wing system with unknown output disturbances and references
International Journal of Robust and Nonlinear Control, 2023For a flexible wing system, two different exosystems are used to generate unknown references and output disturbances, respectively. The wing system is further perturbed by unknown distributed and boundary disturbances that have the same frequencies to ...
Tingting Meng +3 more
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This paper presents applying reinforcement learning to find the optimal sensor/actuator placement (OSAP) policy and optimal control for the flexible wing.
Tianyi He, W. Su
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Dynamical Modeling and Boundary Vibration Control of a Rigid-Flexible Wing System
IEEE/ASME transactions on mechatronics, 2020A boundary control approach is used to control a two-link rigid-flexible wing in this article. Its design is based on the principle of bionics to improve the mobility and the flexibility of aircraft.
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