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All Journal Jurnal Pengabdian Masyarakat Sains Indonesia (Indonesian Journal Of Science Community Services) Vocatech : Vocational Education and Technology Journal
Wahju Santoso, Djarot
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Civil Engineering, Building, Construction & Architecture Computer Science & IT Economics, Econometrics & Finance Education Electrical & Electronics Engineering Library & Information Science Mechanical Engineering Public Health Social Sciences

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ANALISIS KINEMATIK MANUVER TERBANG VERTIKAL PADA KOMPONEN SWASH PLATE, ROTOR HEAD DAN ROTOR BLADES HELIKOPTER SEJENIS NBO - 105 MENGGUNAKAN CATIA V5R16 Sukhairi, Teuku Arriessa; Harahap, Jagodang; Wahju Santoso, Djarot
VOCATECH: Vocational Education and Technology Journal Vol 4, No 2 (2023): April
Publisher : Akademi Komunitas Negeri Aceh Barat

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.38038/vocatech.v4i2.114

Abstract

Helicopters have a unique advantage over airplanes in that they can adjust the direction of their blades to generate lift in any direction, allowing them to perform vertical takeoffs and landings and hover in one spot. This capability makes them highly valuable for a variety of operations, including transportation. A crucial component in the helicopter control system is the swash plate, which allows for adjustments to the angle of the rotor blades to achieve specific maneuvers.To manufacture and model components such as the swash plate, rotor head, and rotor blades, CATIA V5R16 software can be used. This involves modeling the individual parts in the workbench part design, assembling them in the workbench assembly design, or conducting kinematic analysis using the DMU Kinematics workbench to obtain values for linear velocity, angular velocity, linear acceleration, and angular acceleration. When compared to manual calculations, the differences between the results produced by the CATIA V5R16 software and theoretical calculations are negligible. Therefore, it can be concluded that CATIA V5R16 software is highly capable and suitable for conducting kinematic analysis of three-dimensional components.
Simulator Respon Pesawat Berbasis Mikrokontroler: Media Edukatif bagi Siswa dan Komunitas Radio Kontrol Junaidin, Buyung; Wahju Santoso, Djarot; Sudibya, Bambang; Prakoso, Agung; Tri Wahyudi, Makus
Jurnal Pengabdian Masyarakat Sains Indonesia (Indonesian Journal Of Science Community Services) Vol. 7 No. 2 (2025): Desember
Publisher : Universitas Mataram

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.29303/jpmsi.v7i2.1556

Abstract

Interactive learning media are essential in aerospace engineering education, particularly for understanding flight control systems that are difficult to grasp through theory alone. Aircraft responses to aileron, elevator, and rudder deflections require clear visualization to help learners connect control inputs with changes in aircraft attitude. To address this need, this community service program developed a microcontroller-based aircraft response simulator equipped with an attitude sensor as an educational tool for students and radio control (RC) enthusiasts. The microcontroller processes real-time data from an Inertial Measurement Unit (IMU) and displays the aircraft’s attitude angles (yaw, pitch, and roll) on an LCD screen, allowing participants to directly observe how control inputs influence attitude changes. The miniature aircraft responds according to the displayed attitude angles, enabling learners to better understand the relationship between control inputs and aircraft dynamics. Evaluation results show that the simulator operates reliably, provides accurate attitude information, and significantly enhances participants’ understanding of flight control concepts and attitude dynamics. Users also reported that the simulator is easy to operate, engaging, and effective for foundational training in RC aviation. Thus, the microcontroller and IMU-based simulator serves as a practical, replicable, and modern learning medium aligned with contemporary aerospace education.
Co-Authors Agung Prakoso Bambang Sudibya, Bambang Buyung Junaidin, Buyung Harahap, Jagodang Sukhairi, Teuku Arriessa Tri Wahyudi, Makus