SISTEM BUS ELEKTRONIK INASAT-1
| Main Authors: | Abdul Karim, Arbai Yusuf, Dwiyanto; |
|---|---|
| Format: | Book |
| Bahasa: | ind |
| Terbitan: |
LAPAN
, 2005
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| Subjects: | |
| Online Access: |
http://repository.lapan.go.id//index.php?p=show_detail&id=4994 http://repository.lapan.go.id//lib/phpthumb/phpThumb.php?src=../../images/docs/prosiding_workshop_dan_seminar_nasional.PNG.PNG |
Daftar Isi:
- Abstrak Inasat-1 adalah satelit LEO yang mempunyai misi Spacecraft Engineering Test Satellite. Sistem bus elektronik yang didesain selain sebagai penggerak satelit juga berperan sebagai payload demontrasi untuk tnenguli kelavakan desain satelit Inasat-1. Didasarkan misinya Inasat-1 dilengkapi dengan heherapa subsistem yang mendukung kinerjanya satelit. Subsistem yang mendukung Inasat-1 adalah subsistem Electronic Power System (EPS). Onboard Data Handling (OBDH). subsistem Telemetry and Tele Command (770. subsistem Structure dan Attitude Control. Abstract Inasat-1 is that LEO satellite have Spacecraft Engineering mission Test Satellite. Electronic bus system which is didesain besides as sateuite,activator also personate demontrasi payload to test elegihility of Inasal-1 satellite desain. Based by its mission of Inasat-1 provided with some subsistem upporting its performance of satellite. Subsistem supporting Inasat-1 is Electronic Power System (EPS), Onboard Data Handling (OBDH). Telemetry Tele Command (TIC), and Structure and .1ttitude Control. Subsystem. Kata kunci : EPS, OBDH, TTC, Inasat-1
- Hlm. 91-100