Dynamic stability in vertically flying insect-mimicking flapping wing system

L. T. K. Au, H. Phan, A. Budiyono, H. Park
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引用次数: 1

Abstract

This paper provides a quantitative analysis for the longitudinal dynamic stability of a vertically flying insect-mimicking flapping wing system (FWS. In order to define the parameters in the equation of motion, the computational fluid dynamics (CFD) by ANSYS-Fluent was used. The aerodynamic forces and moment when the FWS was installed vertically and then inclined -15 and +15 degree for flight speeds of 0, 0.2 and 0.4 rn/s were computed. Through the eigenvalue and eigenvector analysis of the system matrix, we could make the formal description of the dynamic stability of the FWS. Three modes of motion were identified: one stable oscillatory mode, one unstable divergence mode, and one stable subsidence mode. Due to the divergence mode, the FWS eventually becomes unstable. However, the FWS could stay stable in the vertical flight during the first 0.5 second.
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垂直飞行仿昆虫扑翼系统的动态稳定性
本文对垂直飞行的仿昆虫扑翼系统(FWS)纵向动力稳定性进行了定量分析。为了确定运动方程中的参数,采用了ANSYS-Fluent计算流体动力学(CFD)软件。计算了飞行速度分别为0、0.2和0.4 rn/s时,FWS垂直安装后再倾斜-15度和+15度时的气动力和力矩。通过对系统矩阵的特征值和特征向量分析,可以形式化地描述系统的动态稳定性。确定了三种运动模式:稳定振荡模式、不稳定发散模式和稳定沉降模式。由于散度模式的存在,FWS最终变得不稳定。然而,在垂直飞行的前0.5秒内,FWS可以保持稳定。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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