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All Journal JETT (Jurnal Elektro dan Telekomunikasi Terapan) Ensiklopedia of Journal Journal of Comprehensive Science ARZUSIN: Jurnal Manajemen dan Pendidikan Dasar Innovative: Journal Of Social Science Research Jurnal Teknologi dan Vokasi Jurnal Multidisiplin Teknologi dan Arsitektur Kohesi: Jurnal Sains dan Teknologi JECCOM Journal of Accounting Law Communication and Technology Journal of Humanities Education Management Accounting and Transportation
Andi Syofian
Institut Teknologi Padang
Religion Arts Humanities Biochemistry, Genetics & Molecular Biology Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Economics, Econometrics & Finance Education Electrical & Electronics Engineering Energy Engineering Languange, Linguistic, Communication & Media Law, Crime, Criminology & Criminal Justice Library & Information Science Nursing Physics Public Health Social Sciences Transportation Other

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PENINGKATAN PERFORMANSI MANUVER GERAKAN ROLL HEXACOPTER DENGAN METODA KENDALI PID ADAPTIF Al, Al; Premadi, Aswir; Effendi, Asnal; Alfith, Alfith; Dasman, Dasman; Syofian, Andi
Jurnal Teknologi dan Vokasi Vol 1 No 2 (2023): Jurnal Teknologi dan Vokasi
Publisher : ITP Press

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.21063/jtv.2023.1.2.75-82

Abstract

In the Hexacopter flight control system, there are three very influential movements, namely Pitch, Roll and Yaw movements. Roll movement is very important to note because it affects the direction of the plane's flight. This movement is strongly influenced by the system's dynamic response to changes in hardware characteristics and the influence of changes in wind direction and speed from external systems. For this reason, this research is offered to implement a control system that can adapt to these dynamic disturbances. This study proposes the application of a proportional integral derivative (PID) control system, where constant values can adjust to dynamic changes in the system. These constant values can adjust to changes in errors and delta errors at any time. then a fuzzy logic controller (FLC) algorithm is applied, to make the constant values adaptable. The design of Fuzzification and Defuzzification is based on the maximum error and delta error limits. After real-plant testing, system performance is obtained as follows: settling time = 24mS; peak time 21mS; rise time = 9mS; delay time = 4.4mS; percent overshoot and steady state error = 1%.
Co-Authors AA Sudharmawan, AA Al Al Al Al Alfiansyah, Fahmi Alfith Alfith Antonov Antonov Anugrah, Anggun Arfita Yuana Dewi Asnal Effendi Aswir Premadi Dasman Dasman Dewan, Muhammad Erhaneli, Erhaneli Fadila, Afif Fajrin, Ridho Hidayat, Rezi kartiria4, kartiria Lufti, Jimmy Al Kito Marsadi, Handrifan Masta, Putra Fikrianda Maulana, Febryan Abdi Nur, Andi M. Nurwijayanti Perdana Putera, Perdana Putra, Andi M. Nur Rachman, Arfita Yuana Dewi Rahman, Aldito Rizki, Muhammad Rizki Saputra, Falmi Ade Sepannur Bandri Sepanur Bandri, Sepanur Sidiq, Rasyid N Sitti Amalia Tanjung, Nabila Marito Usman, Gabriel Hafizh Wibowo, Tiur Lestari Yultrisna Yultrisna Yusreni Warmi Zuriman Anthony