Background for modeling the dynamic characteristics of advanced spacecraft drives considering the operation of oscillators

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Introduction. Precision elements of the target equipment and sensitive elements of the stabilization and orientation system of the advanced spacecraft are considered in the framework of this research. A method and software for modeling the dynamic characteristics of these elements are developed and validated. At that, the processing data results from the experimental studies on active and passive oscillators are taken into account.Materials and Methods. It is shown how the method of weightlessness provides simulation of the conditions that as much as possible conform to the real-time use of advanced space vehicles, precision structural elements, target equipment and their drives. Schemes of the corresponding experimental facilities are presented. Mathematical modeling methods, techniques of machine mechanics and dynamics are applied. Basic parameters of the proposed design dynamics, which are governing parameters in terms of the implementation of the target functions of the spacecraft, are calculated...

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Amplitude of oscillations, damping ratio, dynamic accuracy, spacecraft, mathematical simulation, method, microperturbation, displacement, precision stabilization, drive, software and algorithmic support, velocity, acceleration, oscillation frequency

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Короткий адрес: https://sciup.org/142221965

IDR: 142221965   |   DOI: 10.23947/1992-5980-2019-19-4-317-327

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