WEIGHT ESTIMATION MODELING OF PROPULSION SYSTEM VARIATIONS FOR VTOL FIXED WING UAV IN PARTICULAR MISSION
VTOL Fixed Wing UAV is an aircraft that consists of 2 flying modes, namely VTOL Flight Mode, which in this case it will always use an Energy Converter in the form of 4 Electric Motors, and Fixed Wing Flight Mode which will always use an Energy Converter in the form of 1 motor (can be Electric Motor...
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Main Author: | Firman Ramanda, Muhammad |
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Format: | Theses |
Language: | Indonesia |
Subjects: | |
Online Access: | https://digilib.itb.ac.id/gdl/view/84367 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
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