OPTIMISASI MANUVER KOREKSI UNTUK MENJAGA WAKTU LOKAL SATELIT LAPAN-A4
To achieve a sun-synchronous orbit (SSO), a satellite orbit needs to have a nodal precession rate value equals to the revolution rate of the Earth to the Sun, which is 360°/year. The nodal precession rate, by using J2 zonal harmonic perturbation, is affected by some orbital element values: semi ma...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/62037 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |