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Reduced-Order Forward Flight Dynamics Models for Dipteran Insects

机译:Dipteran昆虫的减少顺序前向飞行动力学模型

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This study applies an experimentally-derived insect aerodynamics model that includes body egomotion to develop reduced order flight dynamics models appropriate for estimating the sensing and feedback requirements of insect flapping flight. Wing motions of freely flying Calliphorid species in forward flight are digitized using an automated kinematics extraction method. The wring kinematics are used as inputs to the aerodynamic model, and rigid body dynamics used to compute 6DOF flight trajectories. Finally, system identification and numerical perturbation techniques are used to derive reduced order models of the forward flight dynamics. Longitudinal results indicate a pitch damping mode and pitch/surge oscillatory mode similar to hovering dynamics. However, the uncoupled heave damping mode observed in hover now involves all longitudinal states, indicating that heave motion is coupled in forward flight. Lateral-directional results show roll and yaw damping modes as in hover, but the combined roll/yaw damping mode is replaced by an unstable oscillatory mode involving all lateral-directional states in roughly equal proportions.
机译:本研究适用于实验衍生的昆虫空气动力学模型,包括身体象征,以开发适合估算昆虫扑拍飞行的传感和反馈要求的秩序飞行动力学模型。使用自动运动学提取方法向前飞行飞行飞行咔嗒声种类的翼运动。 WRING运动学被用作空气动力学模型的输入,并且用于计算6dof飞行轨迹的刚体动力学。最后,系统识别和数值扰动技术用于导出前向飞行动力学的减少阶模型。纵向结果表示类似于悬停动态的音调阻尼模式和俯仰/浪涌振荡模式。然而,在悬停中观察到的未耦合的升降阻尼模式现在涉及所有纵向状态,表明升降运动在向前飞行中耦合。横向结果显示悬停中的辊和偏航阻尼模式,但组合的辊/偏航阻尼模式由涉及所有横向状态的不稳定振荡​​模式代替大致相等的比例。

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