Application of a Micromechanical Gyroscope for Measuring the Angular Momentum in a Seminatural Modeling of Disturbed Rotation of a Space Probe in the Atmosphere

V. Lyubimov, P.V. Lyubimov
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Abstract

We consider the problem of the experimental determination of the angular momentum induced by disturbing asymmetry torques during the motion of the probe model relative to its center of mass. The aim of the study is to develop a scaled-down model of a space probe for atmospheric descent for seminatural modeling of its motion relative to the center of mass with the measurement of the angular velocity by an on-board MEMS gyroscope. Numerical values of the angular velocity are used to calculate the angular momentum of the model.
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微机械陀螺仪测量角动量在空间探测器大气扰动旋转半自然建模中的应用
本文研究了探针模型在相对于质心运动过程中由扰动不对称力矩引起的角动量的实验测定问题。本研究的目的是开发一个大气下降空间探测器的按比例缩小模型,通过机载MEMS陀螺仪测量其角速度,对其相对于质心的运动进行半自然建模。角速度的数值用于计算模型的角动量。
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