Optimal Sizing Sistem Pesawat Terbang Tanpa Awak Bertenaga Surya Untuk Terbang Autonomous

Afif, Muhammad Faiz (2018) Optimal Sizing Sistem Pesawat Terbang Tanpa Awak Bertenaga Surya Untuk Terbang Autonomous. Undergraduate thesis, Institut Teknologi Sepuluh Nopember.

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Abstract

Saat ini pesawat tanpa awak banyak digunakan dalam berbagai kegiatan, salah satunya dapat digunakan untuk pengindraan jarak jauh, dapat menjadi mobile satelite untuk jaringan komunikasi, serta dapat digunakan dalam pengiriman barang-barang untuk korban bencana di daerah yang susah dijangkau oleh manusia. Proses integrasi tenaga surya ke dalam pesawat tanpa awak menjadi topik yang menarik dalam berbagai riset. Beberapa kegunaan dari integrasi tenaga surya ke dalam pesawat tanpa awak adalah kemungkinan untuk terbang terus menerus dengan sumber energi yang mampu disediakan oleh tenaga surya Metode penyesuaian konfigurasi pesawat diharapkan mampu mendapatkan ukuran pesawat optimum dengan mempertimbangkan lama penerbangan, daya pembangkitan panel surya, beban pesawat, gaya angkat pesawat, gaya dorong pesawat, dan gaya hambat pesawat dengan mengatur variabel luasan panel surya, kapasitas penyimpanan energi listrik, lebar sayap, konfigurasi sistem propulsi, agar didapatkan efisiensi penerbangan yang optimum. Kemudian menganalisis hasil optimasi dengan metode multi-objective genetic algorithm dengan menganalisis resultan gaya pada pesawat, energy balance, dan wing loading. Kemudian dilakukan analisis tambahan dengan menganalisis pengaruh perubahan dari payload, tingkat iradiasi, serta efisiensi panel surya terhadap resultan gaya pada pesawat, energy balance, dan wing loading terhadap konfigurasi pesawat hasil Optimal sizing sistem pesawat terbang tanpa awak bertenaga surya. Hasil optimasi didapatkan konfigurasi optimum pesawat terbang tanpa awak untuk dapat terbang terus menerus. ==================================================================================================== Nowdays, Unmanned Aerial Vehicle (UAV) has many potential application such as remote sensing, mobile satelite for communication network, and delivering disaster relief assistance for victim in remote area. The integration process of solar power into unmanned aircraft has become an interesting topic in various researches. Some of the utility of the integration of solar power into unmanned aircraft is the possibility to fly continuously with energy sources capable of providing solar power without limited energy sources. The aircraft configuration adjustment method is expected to be able to obtain optimum aircraft size considering the duration of flight, solar panel power generation, aircraft load, aircraft lift, aircraft thrust and drag resistance by adjusting variable of solar panel area, electric energy storage capacity, wingspan, configuration of the propulsion system, in order to obtain optimum flight efficiency. From the optimal solution result we analyze airplane force resultant, energy balance and wing loading proportion. Furthormore, this paper analyze effect from changes in payload, iridiance level, and solar panel efficiency from optimum plane configuration. Optimation process result on optimal configuration of unmanned aerial vehicle to flight continously.

Item Type: Thesis (Undergraduate)
Uncontrolled Keywords: UAV, Panel Surya, Optimal sizing
Subjects: T Technology > TK Electrical engineering. Electronics Nuclear engineering
T Technology > TK Electrical engineering. Electronics Nuclear engineering > TK1087 Photovoltaic power generation
Divisions: Faculty of Industrial Technology > Electrical Engineering > (S1) Undergraduate Theses
Depositing User: Muhammad Faiz Afif
Date Deposited: 27 Feb 2018 04:21
Last Modified: 27 Feb 2018 04:21
URI: http://repository.its.ac.id/id/eprint/49419

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