Konseptual Desain Pesawat UAV Meniru Cessna 172 Dengan Konfigurasi Sayap Morphing Untuk Misi Trainer

Mizan Fadhilah (Sekolah Tinggi Teknologi Kedirgantaraan)
Haqqah Risath Mas Intan (Sekolah Tinggi Teknologi Kedirgantaraan)

Journal of Applied Mechanical Technology (JAMET)
Vol 1 No 1 (2022): Journal of Applied Mechanical Technology (JAMET)

The development of UAVs/drones in Indonesia is growing rapidly, as evidenced by many domestically made UAVs/drones, because indeed the existence of these drones can assist human tasks in certain fields, therefore researchers are interested in designing a UAV concept for trainer mission purposes with a morphing wing configuration that will be reserved for novice pilots as a condition for obtaining drone pilot certification. By using calculations using the Anderson method, the output of the calculation will be used as a reference in the preparation and manufacturing of the conceptual design of the aircraft to be made. The initial estimated weight of the Cessna 172 UAV aircraft with a morphing wing configuration for trainer mission purposes is 5.375433 lb with a fuselage length of 5.15304 ft, and a wingspan of 5.266345 ft which is positioned above the fuselage, and is powered by 1 engine motor. brushless of 0.129642 hp