DocumentCode :
663530
Title :
A wing characterization method for flapping-wing robotic insects
Author :
Desbiens, Alexis Lussier ; Yufeng Chen ; Wood, Robert J.
Author_Institution :
Harvard Microrobotics Lab., Harvard Univ., Cambridge, MA, USA
fYear :
2013
fDate :
3-7 Nov. 2013
Firstpage :
1367
Lastpage :
1373
Abstract :
This paper presents a wing characterization method for insect-scale flapping-wing robots. A quasi-steady model is developed to predict passive wing pitching at mid-stroke. Millimeter scale wings and passive hinges are manufactured using the SCM fabrication processes. Flapping experiments at various frequencies and driving voltages are performed to extract kinematics for comparison with the quasi-steady predictions. These experiments examine the validity of the quasi-steady model and demonstrate the robustness of the wing characterization method. In addition, because time-averaged lift and drag are strongly correlated with flapping kinematics, quasi-steady prediction of wing kinematics directly leads to predictions of lift and drag generation. Given a flapping frequency and a driving voltage, the model computes the hinge stiffness that leads to optimal flapping kinematics. This reduces the number of flapping experiments required for wing characterization by a factor of four.
Keywords :
aerospace components; aerospace robotics; drag; elasticity; hinges; robot kinematics; SCM fabrication process; drag generation; flapping-wing robotic insects; hinge stiffness; insect-scale flapping-wing robots; millimeter scale wings; passive hinges; quasisteady model; wing characterization method; wing kinematics; Aerodynamics; Computational modeling; Drag; Fasteners; Insects; Kinematics; Mathematical model;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Robots and Systems (IROS), 2013 IEEE/RSJ International Conference on
Conference_Location :
Tokyo
ISSN :
2153-0858
Type :
conf
DOI :
10.1109/IROS.2013.6696527
Filename :
6696527
Link To Document :
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