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All Journal Al-Fiziya: Journal of Materials Science, Geophysics, Instrumentation and Theoretical Physics JOURNAL ONLINE OF PHYSICS Jurnal INSYPRO (Information System and Processing) JURNAL INSTEK (Informatika Sains dan Teknologi) Jurnal Teknologi Dirgantara Jurnal Fisika dan Terapannya AL-KHAZINI: JURNAL PENDIDIKAN FISIKA Jurnal Fokus Elektroda (Energi Listrik, Telekomunikasi, Komputer, Elektronika dan Kendali)
Prasepvianto Estu Broto
Universitas Islam Negeri Alauddin Makassar
Aerospace Engineering Chemical Engineering, Chemistry & Bioengineering Computer Science & IT Control & Systems Engineering Earth & Planetary Sciences Education Electrical & Electronics Engineering Energy Engineering Materials Science & Nanotechnology Mechanical Engineering Physics

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Journal : Jurnal Fisika dan Terapannya

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SIMULASI HARDWARE IN THE LOOP UNTUK TAKE-OFF DAN LANDING OTOMATIS PADA QUADROTOR MENGGUNAKAN PIXHAWK DAN jMAVSim Prasepvianto Estu Broto; Ihsan Ihsan
JFT : Jurnal Fisika dan Terapannya Vol 7 No 2 (2020): DESEMBER
Publisher : Universitas Islam Negeri Alauddin Makassar

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.24252/jft.v7i2.18513

Abstract

The use of quadrotors in various applications has made development and research in the field of drones grow rapidly. In the research and development process, a testing phase is needed to determine the flying attitude of the quadrotor. Live testing can be risky if something goes wrong. With Hardware in The Loop Simulation, it can be used as a way to minimize the occurrence of these errors. Hardware in The Loop Simulation is a combination of software and hardware simulation. The jMAVSim simulation software is connected to the Pixhawk autopilot and ground control station. The simulation results that have been obtained make it possible to carry out direct testing on the Pixhawk autopilot. From this study, the results of the quadrotor flying attitude during take-off and landing simulations show that the quadrotor is still in a stable condition with changes in pitch and roll angles of less than 1 degree.
Co-Authors A. Muhammad Syafar Abu Ammar Hernawati IHSAN IHSAN Ihsan Ihsan Jefri Abner Hamonangan Muh. Said L Muhammad Yusril Nidya Lena Fitriah Laksana Nurul Fuadi PRASEPVIANTO ESTU BROTO Rahmaniah Rahmaniah Rani, Sefrilita Risqi Adikaning