Method for controlling the frequency of eigentones for determination of the astronaut's body weight and small weight in weightlessness

O. Kolomiitsev, Volodymyr Komarov, O. Dmitriiev, V. Pustovarov, R. Oliinyk
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Abstract

In the article the analysis of existent basic methods of determining the weight of body of cosmonauts and objects small weight is conducted in the conditions of weightlessness, and their features of application are similarly exposed. The most comfortable and perspective method of determining the inertial weight of body in the conditions of weightlessness the use of different sort of oscillators and devices, that allow to measure the parameters of body of cosmonaut (small weight of devices and others like that), that hesitates, is considered. It is possible to use dependence of period of vibrations of spring on b.w. of cosmonaut envisaged on her and others like that. The measuring device of weight of «ИМ-01М», his technical descriptions, composition and principle of action, is considered. Such measuring device it maybe to complement the system of weighing of astronauts and cosmonauts on the method of Karmelo Velardo, that allows to get measuring (form and sizes of cosmonaut and his motions) given about the depth of object. The object of research is oscillators and devices, that allow to measure parameters bodies of cosmonaut and objects small weight, that hesitate. The subject of research is a mathematical vehicle on determination of frequency of eigentones dynamic system. The research aims is development of method of control of frequency of eigentones for determining the weight of body of cosmonaut and objects small weight in the conditions of weightlessness. Conclusions. The method of determining the weight of body of cosmonauts and objects small weight in the conditions of weightlessness and method of his realization are offered on the change of frequency of eigentones dynamic system devices. Analytical expressions for the calculation of frequency of eigentones dynamic system devices and corresponding charts are presented. A spring-gravimetric device is worked out for realization of measuring. A chart technical decision over of device is brought, his composition and principle of action are exposed. A device is able to define weight of control object, his state (his heterogeneity, presence of liquid filler, parts that hesitate and others like that).
失重状态下测定宇航员体重和小体重本征音频率的控制方法
本文分析了在失重状态下确定宇航员和小重量物体体重的现有基本方法,并对其应用特点进行了类似的探讨。在失重条件下,确定物体惯性重量的最舒适和最直观的方法是使用不同类型的振荡器和设备,以测量宇航员的身体参数(小重量的设备和其他类似的设备),这是值得考虑的。可以使用弹簧振动周期对她和其他类似人设想的宇航员体重的依赖性。考虑了«ИМ-01М»的重量测量装置及其技术说明、组成和作用原理。这种测量设备可能是对Karmelo Velardo方法的宇航员和宇航员称重系统的补充,该方法可以测量物体的深度(宇航员的形状和大小及其运动)。研究的对象是振荡器和设备,可以测量宇航员的身体和小重量、犹豫的物体的参数。本课题是一个确定本征音动力系统频率的数学工具。本研究的目的是开发在失重条件下确定宇航员和小重量物体重量的本征音频率控制方法。结论。介绍了在失重状态下确定宇航员和小重量物体的体重的方法以及在本征音动态系统装置频率变化的情况下实现的方法。给出了本征音动态系统器件频率计算的解析表达式和相应的图表。为了实现测量,研制了一种弹簧称重装置。给出了该装置的图形技术决策,揭示了其组成和作用原理。一个设备能够定义控制对象的重量、他的状态(他的异质性、液体填充物的存在、犹豫的零件和其他类似的东西)。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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CiteScore
0.50
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0.00%
发文量
47
审稿时长
5 weeks
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