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- W2888892320 abstract "The dynamic study and wing control of an ornithopter autonomous robot in level flight was carried out in this work. A rigid flat plate attached to the bird’s body by a spherical joint was adopted as wing model, conferring three degrees of freedom for the system. To model the flight dynamics and wing motion, the hypothesis that the bird was flying at a constant velocity in an horizontal rectilinear trajectory was used. From the definition of the model to be studied, the equations related to kinematics and dynamics of the mechanism were determined. For the control, the feedback linearization control method was used. Based on the results obtained, it can be concluded that the proposed method is able to control the studied system efficiently. The responses of the control system indicate that partial compensation will provide a decrease in the use of computational resources without degrading the desired response. Modeling and all simulations were implemented in MATLAB and Simulink software." @default.
- W2888892320 created "2018-09-07" @default.
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- W2888892320 date "2018-08-28" @default.
- W2888892320 modified "2023-10-15" @default.
- W2888892320 title "Proposed control for wing movement, type flat plate, for ornithopter autonomous robot" @default.
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- W2888892320 doi "https://doi.org/10.1007/s40430-018-1362-7" @default.
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