HIL Experimental Analyses of Satellite Electrical Power Subsystem (EPS) in De-tumbling Mode
In this study, hardware in the loop (HIL) simulation consisting of solar array simulator, programmable electric load, charger board, distribution board and attitude and position simulator is designed and developed for the mentioned purpose. Because of satellite high angular velocity in de-tumbling m...
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| Главные авторы: | , , , |
|---|---|
| Формат: | Artigo |
| Язык: | Persa |
| Опубликовано: |
Aerospace Research Institute
2018-02-01
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| Серии: | فصلنامه علوم و فناوری فضایی |
| Предметы: | |
| Online-ссылка: | https://jsst.ias.ir/article_59712_04ef7e7d05f23cbee185215145cf3dce.pdf |
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