Control system of spacecraft solar array drive assembly actuator

This paper deals with the issues of developing a control system of a spacecraft solar array drive assembly actuator that meets strict requirements for operation at the set angular accelerations and rotation velocities, under the influence of payload and disturbance forces. The work consists of d...

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Bibliographic Details
Main Authors: D. S. Polozhentsev, D. J. Dzhukich, D. N. Zakharov
Format: Article
Language:English
Published: Omsk State Technical University, Federal State Budgetary Educational Institution of Higher Education 2019-11-01
Series:Омский научный вестник
Subjects:
Online Access:https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/5%20(167)/72-76%20%D0%9F%D0%BE%D0%BB%D0%BE%D0%B6%D0%B5%D0%BD%D1%86%D0%B5%D0%B2%20%D0%94.%20%D0%A1.,%20%D0%94%D0%B6%D1%83%D0%BA%D0%B8%D1%87%20%D0%94.%20%D0%99.,%20%D0%97%D0%B0%D1%85%D0%B0%D1%80%D0%BE%D0%B2%20%D0%94.%20%D0%9D..pdf