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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Bibliographic Details
Main Author: Firman Ramanda, Muhammad
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