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Reduced-Order Forward Flight Dynamics Models for Dipteran Insects

机译:Dipteran昆虫的降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:这项研究应用了包括身体自我运动在内的实验性昆虫空气动力学模型,以开发降阶飞行动力学模型,适用于估计昆虫扑动飞行的感测和反馈需求。使用自动运动学提取方法将前向飞行中自由飞行的Calliphorid物种的机翼运动数字化。拧紧运动学用作空气动力学模型的输入,而刚体动力学则用于计算6DOF飞行轨迹。最后,系统识别和数值摄动技术被用来推导前向飞行动力学的降阶模型。纵向结果表明音调阻尼模式和音调/喘振振荡模式类似于悬停动力学。但是,在悬停时观察到的未耦合升沉阻尼模式现在涉及所有纵向状态,这表明升沉运动在前向飞行中是耦合的。横向结果显示了像悬停一样的侧倾和偏航阻尼模式,但是组合的侧倾/偏航阻尼模式被一个不稳定的振荡模式所取代,该振荡模式涉及所有横向状态,并且比例大致相等。

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