PERTURBASI ORBITAL PADA SATELIT LAPAN A2 DAN LAPAN A3 AKIBAT VARIASI KERAPATAN ATMOSFER SAAT TERJADI BADAI GEOMAGNET KELAS KUAT
Determination of orbit and propagation for satellites operating in low Earth orbit (LEO) need to consider the effects of atmospheric drag, which depend on solar activity expressed in index F10.7 and geomagnetic activity expressed in index Dst. Atmospheric density data used the atmospheric model MSIS...
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Format: | Final Project |
Language: | Indonesia |
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Online Access: | https://digilib.itb.ac.id/gdl/view/47762 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |