ANALISIS WEIGHT AND BALANCE PADA AMF – 16 IF PESAWAT UAV
PENYEMPROT TANAMAN BERBASIS QUADCOPTER
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
Berlian Kusuma Amelia, Chindria
Subject
T Technology (General)
Datestamp
2024-04-26 06:40:43
Abstract :
Weight is the weight of the aircraft while balance refers to location from the center of gravity on the plane. Added various innovations to the aircraft UAVs can cause their center of gravity to change, this too resulting in changes in the balance point that can cause effects in addition to the response of the control system of the UAV aircraft. The aim of this study determine the value of the center of gravity (CG), carry out comparative calculations center of gravity (CG) between numerical methods by modeling on CATIA application and analytical method using the formula for determining the center of gravity with the help of the OCTAVE application, and find out the magnitude of the shift value center of gravity (CG) when the weight is empty, the system is installed, and condition of being given a payload on a plant-based UAV sprayer AMF-16 IF quadcopter. To get the value from calculating the center of gravity (CG) data obtained from direct measurements and modeling in CATIA. Datum The assembly is placed at the left end of sprayer arm 1 (left sprayer arm). Where the front plane is marked by the presence of a pipe on one side The water tank that is the front of the UAV quadcopter aircraft. From the research results, the CG value obtained by manual calculation (CG method analytical) when the empty weight on the axis is (X=552.51 mm, Y=0.01, Z=142.58), when system is installed on the axis (X=582.1 mm, Y=0.051521, Z=154.58), and when given a payload on the axis (X=570.61 mm, Y=0.03097, Z=119.55). Got it also the modeling CG value (CG numerical method) when the empty weight is on the axis (X=552.419 mm, Y=0.03097, Z=119.55), when the system is installed on the axis (X=556.101 mm, Y=0.051, Z=167.238), and when given a payload on the axis (X=554.992 mm, Y=0.031, Z=126.495).
Weight is the weight of the aircraft while balance refers to location from the center of gravity on the plane. Added various innovations to the aircraft UAVs can cause their center of gravity to change, this too resulting in changes in the balance point that can cause effects in addition to the response of the control system of the UAV aircraft. The aim of this study determine the value of the center of gravity (CG), carry out comparative calculations center of gravity (CG) between numerical methods by modeling on CATIA application and analytical method using the formula for determining the center of gravity with the help of the OCTAVE application, and find out the magnitude of the shift value center of gravity (CG) when the weight is empty, the system is installed, and condition of being given a payload on a plant-based UAV sprayer AMF-16 IF quadcopter. To get the value from calculating the center of gravity (CG) data obtained from direct measurements and modeling in CATIA. Datum The assembly is placed at the left end of sprayer arm 1 (left sprayer arm). Where the front plane is marked by the presence of a pipe on one side The water tank that is the front of the UAV quadcopter aircraft. From the research results, the CG value obtained by manual calculation (CG method analytical) when the empty weight on the axis is (X=552.51 mm, Y=0.01, Z=142.58), when system is installed on the axis (X=582.1 mm, Y=0.051521, Z=154.58), and when given a payload on the axis (X=570.61 mm, Y=0.03097, Z=119.55). Got it also the modeling CG value (CG numerical method) when the empty weight is on the axis (X=552.419 mm, Y=0.03097, Z=119.55), when the system is installed on the axis (X=556.101 mm, Y=0.051, Z=167.238), and when given a payload on the axis (X=554.992 mm, Y=0.031, Z=126.495).
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