Dayyan Hanif, . (2024) Rancang Bangun Autonomous Soaring UAV Surveillance (Fixed Wing Type). S1 thesis, Fakultas Teknik Universitas Sultan Ageng Tirtayasa.

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Abstract

Rancang Bangun Autonomous Soaring UAV Surveillance (Fixed Wing Type) Dibutuhkan suatu penghematan pada UAV bertipe pesawat, soaring merupakan solusi penghematan energi tersebut. Skripsi ini membahas penghematan energi surveillance fixed wing UAV. Diracang berdasarkan SB-XC Glider, Intellegent Navigation System for Aerial Vehicles (INAV) sebagai firmware-software, dan dengan metode penerbangan loiter soaring berdasarkan kuncian posisi Global Positioning System (GPS), serta memiliki fitur waypoint mode diminimum ketinggian 400m dari hasil soaring. Hasilnya static loiter radius 60m lebih efektif dibandingkan 30m, performa penghematan tertinggi dengan durasi 47,7menit, 30,2km distance, konsumsi baterai 2,8Ah/jam, efisiensi energi 167,73%, peningkatan 109,24%, dan mengalami penghematan 85,135% (normal vs soaring), serta mean error navigasi Latitude 6,009% dan Longitude 2,153%. Kata Kunci: Kendali otonom, Sistem jarak jauh, Sistem kecerdasan navigasi untuk kendaraan udara (INAV), Pesawat pengawas tanpa awak, Pesawat layang Autonomous Soaring UAV Surveillance Design (Fixed Wing Type) Savings are needed on aircraft type UAVs, soaring is an energy saving solution. This thesis discusses energy savings for surveillance fixed wing UAVs. Designed based on the SB-XC Glider, Intelligent Navigation System for Aerial Vehicles (INAV) as firmware-software, and with a loiter soaring flight method based on Global Positioning System (GPS) position locking, also has a waypoint mode feature with a minimum altitude of 400m from the soaring results. The result is that a static loiter radius of 60m is more effective than 30m, the highest saving performance with a duration of 47.7 minutes, 30.2km distance, battery consumption of 2.8Ah/hour, energy efficiency of 167.73%, an improvement of 109.24%, and a savings of 85.135% (normal vs soaring), and the mean navigation error for Latitude is 6.009% and Longitude is 2.153%. Keywords: Autonomous, Long range system, Intelligent Navigation System for Aerial Vehicles (INAV), Surveillance UAV, Soaring glider

Item Type:	Thesis (S1)
Contributors:	Contribution Contributors NIP/NIM Thesis advisor Dr. Romi Wiryadinata, S.T., M.T, . 198307032009121006 Thesis advisor Fadil Muhammad, S.T., M.T, . 199104172019031013 Thesis advisor Imamul Muttakin, S.T., M.Eng. Ph.D, . 198705262014041001 Thesis advisor Cakra Adipura W, S.T., M.T, . 199006282019031010 Scientific advisor Prof. Jack W. Langelaan, B.Sc., M.Sc., Ph.D, . UNSPECIFIED
Subjects:	Q Science > Q Science (General) Q Science > QA Mathematics Q Science > QA Mathematics > QA75 Electronic computers. Computer science Q Science > QA Mathematics > QA76 Computer software Q Science > QC Physics T Technology > T Technology (General) T Technology > TJ Mechanical engineering and machinery T Technology > TK Electrical engineering. Electronics Nuclear engineering T Technology > TL Motor vehicles. Aeronautics. Astronautics T Technology > TR Photography T Technology > TS Manufactures T Technology > TT Handicrafts Arts and crafts T Technology > TX Home economics U Military Science > U Military Science (General)
Divisions:	03-Fakultas Teknik > 20201-Jurusan Teknik Elektro
Depositing User:	Dayyan Hanif Hanif
Date Deposited:	09 Aug 2024 09:31
Last Modified:	09 Aug 2024 09:31
URI:	http://eprints.untirta.ac.id/id/eprint/40427

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