2014 IEEE International Conference on Robotics and Automation (ICRA) 2014
DOI: 10.1109/icra.2014.6907372
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A hybrid dynamic model for bio-inspired soft robots — Application to a flapping-wing micro air vehicle

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Cited by 13 publications
(31 citation statements)
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“…The considered robot is composed of a rigid thorax and two soft wings whose the deformations are concentrated along the leading edge (see figure 1). In order to model such a soft system, we propose, as [14], to discretize each wing of the robot in a serial assembly of M planar rigid sections connected together by a 1-DoF angular joint aligned with the leading edge. The model of twisting is linear with stiffness coefficient K e and damping coefficient K v .…”
Section: A Parametrisation and Notationsmentioning
confidence: 99%
“…The considered robot is composed of a rigid thorax and two soft wings whose the deformations are concentrated along the leading edge (see figure 1). In order to model such a soft system, we propose, as [14], to discretize each wing of the robot in a serial assembly of M planar rigid sections connected together by a 1-DoF angular joint aligned with the leading edge. The model of twisting is linear with stiffness coefficient K e and damping coefficient K v .…”
Section: A Parametrisation and Notationsmentioning
confidence: 99%
“…α measures the height of the connection point of the actuated joints above the ellipsoidal body's Center of Mass (CoM). design of the MAV defined in table I [33], and one passive (twisting) joint per wing, cyclic motions have been found for a wing-beat frequency ranging from 7 Hz to 43 Hz. Different hovering flights controlled with the beating law (7), are illustrated on figure 4, which shows the needed amplitude expressed as a function of the frequency.…”
Section: B Hovering Flightmentioning
confidence: 99%
“…Once the motion of the actuated variables is fixed through (7), the motion of the MAV is entirely defined by the initial value of its passive (internal and external) state variables and its dynamic model [33]. Cyclic motion can be obtained through the numerical resolution of the boundaryvalue problem defined in section (III).…”
Section: B Hovering Flightmentioning
confidence: 99%
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