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

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.