日本ロボット学会誌
Online ISSN : 1884-7145
Print ISSN : 0289-1824
ISSN-L : 0289-1824
流体・構造連成シミュレーションによる羽ばたき飛行ロボットの浮上力解析
濱本 将樹太田 佳似原 圭太久田 俊明
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ジャーナル フリー

2007 年 25 巻 6 号 p. 944-950

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Lift force and specification requirements for a dragonfly-scale flapping flight robot are quantitatively investigated by using fluid-structure interaction analysis. For the robotics application of flapping flight, the specifications of actuators and energy sources to generate a certain lift force are essential to design a realistic robot. However, these parameters have been poorly studied because of the difficulty of small-scale unsteady aerodynamics interacting with flapping wings. In the present paper, we show the quantitative evaluation of these parameters in a design of realistic 2DOF actuator by using a fluid-structure interaction analysis based on arbitrary Lagrangian-Eulerian finite element method.
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