PERANCANGAN AWAL TARGET
DRONE AD-05
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Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
BONARDO GIRSANG, RIO
Subject
T Technology (General)
Datestamp
2024-07-29 02:17:51
Abstract :
Drone Target is a vehicle that looks like an aircraft which can operate without pilot inside it, it is controlled by remote. The drone target has a mission as a shooting target, so it is very appropriate to be used as a military aid in shooting exercises. This study aims to discuss the initial compounding of a drone target, including getting configuration and modeled in 3 dimensions, aerodynamic characteristics, range and endurance and static stability of the drone target be named AD-05. The writing of this scientific work specially discuss the initial design of the AD-05 Drone Target use literature study methods and interviews from the experts. In the design process carried out, there are three softwares used: CATIA, ANSYS, and XFLR5. CATIA software is used for modeling aircraft in 3-dimensional form, ANSYS software is used to find the aerodynamic characteristics of the aircraft design, XFLR5 software is used to simulate static stability of the planes. After calculate the geometry, aerodynamic characteristics, range and endurance and static stability analysis, the results of the AD-05 Drone Target have a maximum weight is 71.654 kg with 3 m of span length, 55.56 m / s of flight speed, aerodynamic characteristics that are expected can fly the Drone Target AD-05, and the maximum flight time is 60.705 minutes with 309.577 km of maximum flight distance, but the AD-05 Drone Target has not met the requirements for static longitudinal stability.
Drone Target is a vehicle that looks like an aircraft which can operate without pilot inside it, it is controlled by remote. The drone target has a mission as a shooting target, so it is very appropriate to be used as a military aid in shooting exercises. This study aims to discuss the initial compounding of a drone target, including getting configuration and modeled in 3 dimensions, aerodynamic characteristics, range and endurance and static stability of the drone target be named AD-05. The writing of this scientific work specially discuss the initial design of the AD-05 Drone Target use literature study methods and interviews from the experts. In the design process carried out, there are three softwares used: CATIA, ANSYS, and XFLR5. CATIA software is used for modeling aircraft in 3-dimensional form, ANSYS software is used to find the aerodynamic characteristics of the aircraft design, XFLR5 software is used to simulate static stability of the planes. After calculate the geometry, aerodynamic characteristics, range and endurance and static stability analysis, the results of the AD-05 Drone Target have a maximum weight is 71.654 kg with 3 m of span length, 55.56 m / s of flight speed, aerodynamic characteristics that are expected can fly the Drone Target AD-05, and the maximum flight time is 60.705 minutes with 309.577 km of maximum flight distance, but the AD-05 Drone Target has not met the requirements for static longitudinal stability.
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