PEMODELAN DINAMIKA STRUKTUR DAN IMPLEMENTASI AWAL KENDALI AKTIF PEREDAMAN GETARAN UNTUK WAHANA ANTARIKSA FLEKSIBEL
In this research, vibration on the spacecraft’s structure is occurs due to the spacecraft attitude and its operational condition on a certain orbit. The model of spaceraft’s solar panel is modelled by selecting the typical value of natural frequency and it’s studied by using its flexibel equation of...
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| 主要作者: | |
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| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/54869 |
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