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Analysis of spacecraft actuator mechanisms design process using tensor method

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, , Citation N A Testoedov et al 2018 IOP Conf. Ser.: Mater. Sci. Eng. 450 042003 DOI 10.1088/1757-899X/450/4/042003

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levko@sibsau.ru

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1 JSC "Academician M F Reshetnev Information satellite systems", 52 Lenin street, Zheleznogorsk, Krasnoyarsk region, 662972, Russia

2 JSC "Central Construction Bureau "Geofizika", 89 Kirenskogo street, Krasnoyarsk, Russia

3 Reshetnev Siberian State University of Science and Technology, 31, Krasnoyarsky Rabochy Av., Krasnoyarsk, 660037, Russia

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1757-899X/450/4/042003

Abstract

There is high topicality of more and more complicated systems analysis currently. One of the means to do such analysis is to use Gabriel Kron tensor method. The process of spacecraft driving gear design is analysed by using tensor method. The problematic stages of the process are determined.

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10.1088/1757-899X/450/4/042003