PROSES MANUFAKTUR DAN PERHITUNGAN CENTER OF
GRAVITY (CG) PESAWAT UAV V-SKY 14 NG
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
SYUKUR RAHMADI, MUHAMMAD
Subject
T Technology (General)
Datestamp
2024-07-19 08:28:45
Abstract :
Unmanned aerial vehicle (UAV) is an aircraft that can carry out flight missions by being controlled on electronic devices without a pilot in the aircraft, with the development of UAV technology that is increasingly advanced and growing rapidly, UAV technology has been widely applied for vertical take off and landing (VTOL) environmental monitoring. In writing this thesis, we discuss the manufacturing and determination of the center of gravity (CG) on the UAV V-SKY 14 NG aircraft which has a mission to monitor road traffic. In the manufacturing process of the UAV V-SKY 14 NG aircraft using conventional and non-conventional methods using styrofoam, carbon pipe, plywood and laminating paper. The convetional methods used in manufacturing UAV V-SKY 14 NG include hot wire cutting, cutting using cutters, hacksaw, and finishing using sandpaper, while non-conventional methods are used for laser cutting and 3D printing. After the aircraft is finished manufacturing, it is weighed and measured the arm to calculate the weight and balance on the aircraft. The manufacturing process for the UAV V-SKY 14 NG includes cutting malls, manufacturing fuselage, wings, tail booms, vertical and horizontal stabilizers, VTOL rods, several additional parts such as wing locks with bolted connectors. The results from the manufacturing show that the V-SKY 14 NG UAV has a design dimensional deviation level with actual manufacturing with a precise, medium, and rough level of deviation, has a center of gravity location at 360.5 mm from the datum (nose) or 26.5% of MAC. (wings).
Unmanned aerial vehicle (UAV) is an aircraft that can carry out flight missions by being controlled on electronic devices without a pilot in the aircraft, with the development of UAV technology that is increasingly advanced and growing rapidly, UAV technology has been widely applied for vertical take off and landing (VTOL) environmental monitoring. In writing this thesis, we discuss the manufacturing and determination of the center of gravity (CG) on the UAV V-SKY 14 NG aircraft which has a mission to monitor road traffic. In the manufacturing process of the UAV V-SKY 14 NG aircraft using conventional and non-conventional methods using styrofoam, carbon pipe, plywood and laminating paper. The convetional methods used in manufacturing UAV V-SKY 14 NG include hot wire cutting, cutting using cutters, hacksaw, and finishing using sandpaper, while non-conventional methods are used for laser cutting and 3D printing. After the aircraft is finished manufacturing, it is weighed and measured the arm to calculate the weight and balance on the aircraft. The manufacturing process for the UAV V-SKY 14 NG includes cutting malls, manufacturing fuselage, wings, tail booms, vertical and horizontal stabilizers, VTOL rods, several additional parts such as wing locks with bolted connectors. The results from the manufacturing show that the V-SKY 14 NG UAV has a design dimensional deviation level with actual manufacturing with a precise, medium, and rough level of deviation, has a center of gravity location at 360.5 mm from the datum (nose) or 26.5% of MAC. (wings).
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