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All Journal PROtek Sistemasi: Jurnal Sistem Informasi Jurnal Komputasi Jurnal Tekno Kompak Jurnal ABDINUS : Jurnal Pengabdian Nusantara Jurnal Ilmiah Infrastruktur Teknologi Informasi Journal Social Science And Technology For Community Service JITEL (Jurnal Ilmiah Telekomunikasi, Elektronika, dan Listrik Tenaga) Jurnal Saintekom : Sains, Teknologi, Komputer dan Manajemen Jurnal Inovasi Pembangunan Jurnal Telematics and Information Technology (TELEFORTECH)
Syaiful Ahdan
Universitas Teknokrat Indonesia
Aerospace Engineering Agriculture, Biological Sciences & Forestry Humanities Automotive Engineering Biochemistry, Genetics & Molecular Biology Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Decision Sciences, Operations Research & Management Earth & Planetary Sciences Economics, Econometrics & Finance Education Electrical & Electronics Engineering Energy Engineering Environmental Science Industrial & Manufacturing Engineering Languange, Linguistic, Communication & Media Mathematics Medicine & Pharmacology Nursing Public Health Social Sciences Transportation Other

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Journal : PROtek

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Pengendalian Sikap Lateral Pesawat Flying wing Menggunakan Metode LQR Try Susanto; Syaiful Ahdan
PROtek : Jurnal Ilmiah Teknik Elektro Vol 7, No 2 (2020): PRotek : Jurnal Ilmiah Teknik Elektro
Publisher : Program Studi Teknik Elektro Universitas Khairun

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.33387/protk.v7i2.2034

Abstract

Unnamed Aerial Vehicle (UAV) technology of drone is widely used to carry out various mission such as photography, disaster monitoring, and area mapping. However, crash can be caused by environmental disturbances that hinders the completion of the mission. Moreover, an automatic control system is needed to handle this. In this study, the LQR control method is used to control the eleven and pitch angle so that the drone is able to maintain a stable lateral attitude. This control method has a fast and strong response in reaching a point of balance. Based on the test results, it show that the LQR control method applied is able to control the pitch angle and is able to make the drone maintain a lateral attitude, as evidenced by the disturbance at a pitch 20∘ the drone is able to maintain a lateral attitude with overshoot of 4.23∘, risetime of 0,7 second, settling time of 1,2 second with a steady state error trend of 0,78
Co-Authors Adhie Thyo Priandika Adi Sucipto, Adi Ananda Dika Erlangga Andi Nurkholis Andini Reska Putri Arief Budiman Donaya Pasha Ellin Gusbriana Fransisca Elisabeth Naibaho Hermina Feronika Marpaung Hufajar Wiliam David Jupriyadi, Jupriyadi Kevinda Sari Lintang Sari Dewi Mochamad Susantok Muhammad Aziz Muhammad Diono Muhammad Hamdan Sobirin Muhammad Raihan Putri Indah Sari Rio Andika Sampurna Dadi Riskiono Suci Ramadona Surya Darmansyah Teddy Azidane Tria Setyani Try Susanto Vega Vigia Hanuri Wilga Safira Zahrina Amalia