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Measurement of Flight Dynamics of a Frisbee Using a Triaxial MEMS Gyroscope

机译:使用三轴MEMS陀螺FISBEE的飞行动力学测量

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摘要

A Frisbee with a mass of 0.21 kg, diameter of 0.27 m and moment of inertia (MOI) of 0.002 kg?m2 was instrumented with a triaxial gyroscope. The Frisbee was thrown at low angular velocities as the measurement limit of a single gyroscope was at 6.065 rps. The angular velocities of the triaxial gyroscope were analysed to study the attitude of a Frisbee before and after release. The angular velocities measured were post-processed and the following data were obtained: spin rate at release—3.9–6.14 rps; user-induced peak torque—0.483–0.9 Nm, and peak angular acceleration—204–358 rad/s2; and power input 7.53–19.56 W. The Frisbee wobbled at release which decreased during the flight due to a damping effect. This affected the spin decay, the reduction of wobble lead to a reduced drag force and thus to a smaller spin decay, which was initially 1.12–0.31 rev/s2 and then asymptoted to 0.11–0.01 rev/s2.
机译:质量为0.21千克,直径为0.27米和惯性矩(MOI)的飞碟,用三轴陀螺仪用。由于单个陀螺仪的测量极限为6.065 rps,飞行物被抛出。分析三轴陀螺仪的角速度,以研究释放前后飞盘的姿态。测得的角速度是后处理的,得到以下数据:在释放和mdash时旋转速率; 3.9– 6.14 rps;用户诱导的峰值扭矩和mdash; 0.483– 0.9nm,和峰角加速和mdash; 204– 358 rad / s2;和电源输入7.53– 19.56 W.由于阻尼效果,飞行在飞行期间减少的释放。这影响了旋转衰减,减少摆动导致减少的阻力,从而缩小旋转衰减,最初为1.12和ndash; 0.31 rev / s2,然后渐近至0.11– 0.01 Rev / S2。

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