In the present study, a robotic system is considered: a multi-stage semi-natural simulation stand. The stand is designed to simulate the flight characteristics of aircraft instruments in laboratory conditions. The use of such stands can significantly reduce the cost of developing and testing aircraft instruments and contains all the attributes of robotic systems, which allows the developed method of computer modeling and analysis of stands to be applied in the field of robotic systems. The problem is solved by the finite element method. As a result of the study, a technique has been developed for approximating parts that carry out movements: gear rims, bearings, gearboxes, motors in the finite element method. Comparison with the available experimental studies showed the effectiveness of the developed methodology. As the stand material, a composite material is used, which has a high specific strength, which makes it possible to change the physical and mechanical characteristics depending on the location of the composite base in the layers of the multilayer composite structure. A technique has been developed for arranging the base layers in a multilayer composite to obtain maximum strength and rigidity of the stand, which is one of the main factors in the efficiency of the stand. The analysis of the behavior and stress-strain state of the bench under dynamic impact has been carried out.

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Описана конструкция экспериментальной установки для проведения сравнительных испытаний износостойкости различных пар трения конструкционных материалов. Представлены результаты сравнительных испытаний износостойкости двух пар трения при статическом нагружении и определена лучшая из них. Приведены результаты испытаний износостойкости лучшей пары трения при динамическом нагружении. Разработана математическая модель динамического изнашивания лучшей пары трения конструкционных материалов. The design of an experimental installation for conducting comparative tests of the wear resistance of various friction pairs of structural materials is described. The results of comparative tests of the wear resistance of two friction pairs under static loading are presented and the best of them is determined. The results of tests of the wear resistance of the best friction pair under dynamic loading are presented. A mathematical model of dynamic wear of the best friction pair of structural materials is developed.

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