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This thesis is about validation and aplication of 7orbit. 7orbit itself is a satellite launch vehicle simulation software that developed by LAPAN and ITB in Matlab language as a tool for RPS-530 LAPAN developing. There are three part of this thesis, modification, validation and aplication. The modif...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/17184 |
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| Institution: | Institut Teknologi Bandung |
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id-itb.:171842017-10-09T10:33:26Z#TITLE_ALTERNATIVE# UTAMA (NIM : 13607050); Pembimbing: Dr. Ridanto Eko Poetro, SATRIYA Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/17184 This thesis is about validation and aplication of 7orbit. 7orbit itself is a satellite launch vehicle simulation software that developed by LAPAN and ITB in Matlab language as a tool for RPS-530 LAPAN developing. There are three part of this thesis, modification, validation and aplication. The modification is to support the validation, not to improve or change 7orbit performance. The validation is by simulated flight recorded rocket then compare simulation result with the flight record. The aplication is to develope RPS-530 LAPAN. First, it will simulate the latest configuration of RPS-530 LAPAN, then simulate modificated RPS-530 LAPAN. The simulation result would be used as a consideration for the <br /> <br /> <br /> <br /> <br /> next LAPAN’s satellite launch vehicle. text |
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Institut Teknologi Bandung |
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Institut Teknologi Bandung Library |
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Asia |
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Indonesia Indonesia |
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Institut Teknologi Bandung |
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| language |
Indonesia |
| description |
This thesis is about validation and aplication of 7orbit. 7orbit itself is a satellite launch vehicle simulation software that developed by LAPAN and ITB in Matlab language as a tool for RPS-530 LAPAN developing. There are three part of this thesis, modification, validation and aplication. The modification is to support the validation, not to improve or change 7orbit performance. The validation is by simulated flight recorded rocket then compare simulation result with the flight record. The aplication is to develope RPS-530 LAPAN. First, it will simulate the latest configuration of RPS-530 LAPAN, then simulate modificated RPS-530 LAPAN. The simulation result would be used as a consideration for the <br />
<br />
<br />
<br />
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next LAPAN’s satellite launch vehicle. |
| format |
Final Project |
| author |
UTAMA (NIM : 13607050); Pembimbing: Dr. Ridanto Eko Poetro, SATRIYA |
| spellingShingle |
UTAMA (NIM : 13607050); Pembimbing: Dr. Ridanto Eko Poetro, SATRIYA #TITLE_ALTERNATIVE# |
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UTAMA (NIM : 13607050); Pembimbing: Dr. Ridanto Eko Poetro, SATRIYA |
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UTAMA (NIM : 13607050); Pembimbing: Dr. Ridanto Eko Poetro, SATRIYA |
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| url |
https://digilib.itb.ac.id/gdl/view/17184 |
| _version_ |
1820745551099985920 |