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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| Main Authors: | D. S. Polozhentsev, D. J. Dzhukich, D. N. Zakharov |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Omsk State Technical University, Federal State Autonoumos 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 |
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