Design of Transition Mode Control System of Tilt-Wing UAV
Tilt-Wing UAV (Unmanned Aerial Vehicle) is a type of aircraft which has wing that can be rotated. The tilt-wing mechanism is implemented to increase the performance of the aircraft. This aircraft is capable of doing vertical take-off and landing (VTOL) like a helicopter and flying horizontally like...
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| المؤلف الرئيسي: | |
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| التنسيق: | Final Project |
| اللغة: | Indonesia |
| الوصول للمادة أونلاين: | https://digilib.itb.ac.id/gdl/view/21219 |
| الوسوم: |
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| المؤسسة: | Institut Teknologi Bandung |
| اللغة: | Indonesia |