Flapping-wing robot achieves stable flight through adaptive disturbance control (IMAGE)

Chiba University

Flapping-wing robot achieves stable flight through adaptive disturbance control

Caption

The figure illustrates the process by which the proposed bandwidth-constrained disturbance observer estimates disturbances acting on a flapping-wing micro aerial vehicle and achieves robust position control.

Credit

Assistant Professor Abner Asignacion and Dr. Satoshi Suzuki from Chiba University, Japan

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