PERANCANGAN AWAL PESAWAT UAV UNTUK MISI PENGIRIMAN PAKET PADA WILAYAH KARATINA

Alvionita, Alvionita (2023) PERANCANGAN AWAL PESAWAT UAV UNTUK MISI PENGIRIMAN PAKET PADA WILAYAH KARATINA. Thesis thesis, Institut Teknologi Dirgantara Adisutjipto.

	Text (ABSTRAK) 16050057_ABSTRAK.pdf Download (72kB)
	Text (BAB I) 16050057_ BAB 1.pdf Download (81kB)
	Text (DAFTAR PUSTAKA) 16050057_DAFTAR PUSTAKA.pdf Download (69kB)
	Text (FULL SKRIPSI) 16050057.pdf Restricted to Repository staff only Download (4MB)

Abstract

One of the technological developments in the aviation industry is the manufacture of UAV (Unmanned Aerial Vehicle) aircraft which has undergone several developments, one of which is in terms of materials that have strong properties but are still lightweight, so as to facilitate work. The research objectives are as follows to obtain power loading and wing loading values for predetermined specifications. Obtain the required battery capacity for the vehicle mission with the specified parameters. Get the UAV wing reference geometry. Determine the static stability characteristics of the UAV. XLFR5 is a software for analyzing aircraft stability such as drawings and aircraft force calculations. The results obtained are in the form of wing loading values of 1.814 lb ft ⁄ 2 and wing area values of 1,600 ft2 , Power Loading values of 0.00374 lb/watt , battery capacity of 10.00 Mah, wing reference values sonsisting tapper ratio of 5, MAC is 0.6492 ft, Neutral Point is 0.0349, Nilai X cg is 0.021, Nilai X ct is 0.0821, and UAV stability characteristics obtained are static. The research results can be a reference for subsequent research.

Actions (login required)

View Item

Downloads