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