| NIM | H1A022024 |
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| Namamhs | ADYUTA NAYOTTAMA RAKHA WAHYUDI |
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| Judul Artikel | PERANCANGAN SISTEM KENDALI SERVO PADA PESAWAT AEROMODELLING GLIDER F1A BERBASIS MIKROKONTROLER |
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| Abstrak (Bhs. Indonesia) | Penelitian ini dilatarbelakangi oleh penggunaan timer mekanis berbasis sumbu bakar pada pesawat glider F1A yang memiliki keterbatasan dalam presisi waktu, ketahanan terhadap kondisi lingkungan, serta potensi gangguan mekanis yang memengaruhi performa penerbangan. Penelitian ini bertujuan merancang dan mengimplementasikan sistem kendali multi-servo berbasis mikrokontroler sebagai alternatif timer mekanis untuk mengatur konfigurasi aktuator dan waktu transisi fase penerbangan secara terprogram. Sistem menggunakan Arduino Nano untuk mengendalikan servo rudder, elevator, dan hook melalui sinyal PWM, serta aplikasi Android melalui USB OTG untuk konfigurasi parameter yang disimpan pada EEPROM. Pengujian meliputi komunikasi aplikasi dan EEPROM, akurasi sudut servo, ketepatan durasi, algoritma Safe Zoom, jangkauan receiver determa, dan kinerja penerbangan. Hasil pengujian menunjukkan komunikasi aplikasi dan penyimpanan parameter pada EEPROM berhasil tanpa kegagalan. Servo rudder memiliki rata-rata error 1,50°–2,00%, sedangkan elevator sebesar 0,76%. Transisi fase zoom menghasilkan rata-rata error 9,58%, sedangkan flight time 120 detik memiliki rata-rata error 0,83%. Receiver determa mencapai keberhasilan komunikasi 100% pada jarak 100–600 meter. Lima kali pengujian penerbangan menunjukkan seluruh tahapan berhasil dijalankan sesuai parameter. Sistem mampu menjalankan fungsi timer dan pengendalian fase penerbangan secara otomatis, konsisten, dan dapat dikonfigurasi sebagai alternatif timer mekanis. |
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| Abtrak (Bhs. Inggris) | This research was motivated by the use of a mechanical timer based on a fuse in F1A glider aircraft, which has limitations in timing precision, environmental durability, and potential mechanical failures that may affect flight performance. This research aims to design and implement a microcontroller- based multi-servo control system as an alternative to the mechanical timer for controlling actuator configurations and flight phase transition times. The system uses an Arduino Nano to control rudder, elevator, and hook servos through Pulse Width Modulation (PWM) signals, while an Android application connected via USB On-The-Go (USB OTG) is used to configure parameters stored in EEPROM. Testing included application and EEPROM communication, servo angle accuracy, timing accuracy, the Safe Zoom algorithm, determa receiver range, and flight performance. The results showed successful communication between the application and microcontroller, as well as reliable EEPROM parameter storage and retrieval. The rudder servo achieved an average error of 1.50%–2.00%, while the elevator servo achieved 0.76%. Zoom phase transitions resulted in an average error of 9.58%, while a 120-second flight time showed an average error of 0.83%. The determa receiver achieved 100% communication success at distances of 100– 600 meters. Five flight tests successfully completed all phases according to the configured parameters. The system can therefore serve as an automatic, consistent, and configurable alternative to the mechanical timer. |
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| Kata kunci | multi-servo, mikrokontroler, timer digital, glider F1A, PWM, Aeromodelling |
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| Pembimbing 1 | Ir. Agung Mubyarto, ST., MT. |
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| Pembimbing 2 | Ir. Priswanto, ST., M.Eng , |
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| Pembimbing 3 | |
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| Tahun | 2026 |
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| Jumlah Halaman | 200 |
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| Tgl. Entri | 2026-08-21 11:21:48.168367 |
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