2020 5th International Conference on Advanced Robotics and Mechatronics (ICARM) 2020
DOI: 10.1109/icarm49381.2020.9195327
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A Testing Platform for Flapping-Wing Robots

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Cited by 2 publications
(1 citation statement)
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“…Jones et al [125] devised a rotating arm test stand (figure 18) to measure the lift and thrust of a micro air vehicle with flapping wings. As illustrated in figure 19, in our previous [126] and recent work, we designed an aerodynamics and kinematics testing platform for FWRs, composed of a rotating mechanism, a control system, a force recording system, and a binocular vision system. Compared with the traditional wind tunnel, the platform is more convenient and energysaving in testing the effects of flapping frequency, angle of attack, incoming flow speed, wing folding, and wing deforming on the performance of the FWR.…”
Section: Devices For Simulating Flight Environmentmentioning
confidence: 99%
“…Jones et al [125] devised a rotating arm test stand (figure 18) to measure the lift and thrust of a micro air vehicle with flapping wings. As illustrated in figure 19, in our previous [126] and recent work, we designed an aerodynamics and kinematics testing platform for FWRs, composed of a rotating mechanism, a control system, a force recording system, and a binocular vision system. Compared with the traditional wind tunnel, the platform is more convenient and energysaving in testing the effects of flapping frequency, angle of attack, incoming flow speed, wing folding, and wing deforming on the performance of the FWR.…”
Section: Devices For Simulating Flight Environmentmentioning
confidence: 99%