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Within-wingbeat damping: dynamics of continuous free-flight yaw turns in Manduca sexta

机译:机翼内节拍阻尼:Manduca sexta中连续自由飞行偏航的动力学

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摘要

Free-flight body dynamics and wing kinematics were collected from recordings of continuous, low-speed, multi-wingbeat yaw turns in hawkmoths (Manduca sexta) using stereo videography. These data were used to examine the effects of rotational damping arising from interactions between the body rotation and flapping motion (flapping counter-torque, FCT) on continuous turning. The moths were found to accelerate during downstroke, then decelerate during upstroke by an amount consistent with FCT damping. Wing kinematics related to turning were then analysed in a simulation of hawkmoth flight; results were consistent with the observed acceleration–deceleration pattern. However, an alternative wing kinematic which produced more continuous and less damped accelerations was found in the simulation. These findings demonstrate that (i) FCT damping is detectable in the dynamics of continuously turning animals and (ii) FCT-reducing kinematics do exist but were not employed by turning moths, possibly because within-wingbeat damping simplifies control of turning by allowing control systems to target angular velocity rather than acceleration.
机译:自由飞行的身体动力学和机翼运动学是使用立体影像学从鹰蛾(曼杜卡六倍体)连续,低速,多机翼的偏航转弯记录中收集的。这些数据用于检查车身旋转和拍打运动(拍打反扭矩,FCT)之间的相互作用对连续转弯产生的旋转阻尼的影响。发现飞蛾在下冲程时会加速,然后在上冲程时会减速,其衰减量与FCT阻尼一致。然后在模拟鹰蛾飞行中分析了与转弯有关的机翼运动学。结果与观察到的加减速模式一致。然而,在模拟中发现了一种替代的机翼运动学,该运动学产生了更大的连续性和更少的阻尼加速度。这些发现表明,(i)在连续转弯的动物的动力学中可检测到FCT阻尼,并且(ii)确实存在降低FCT的运动学特性,但飞蛾并未使用它,这可能是因为机翼内部的阻尼通过允许控制系统简化了转弯控制。定位角速度而不是加速度。

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