SIMULASI DAN PERENCANAAN STATION KEEPING SATELIT LAPAN-A4 (SSO) DENGAN MENGGUNAKAN PROPULSI NON-IMPULSIF
Sun-synchronous orbit is an orbit so that the satellite passes over certain region on Earth’s surface at the same local time every day. In order to achieve sun-synchronous orbit, the orbit has to have certain value of nodal precession rate, that is equal to 360°/year. This nodal precession rate is a...
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| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/48271 |
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| 機構: | Institut Teknologi Bandung |
| 語言: | Indonesia |