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All Journal Conference SENATIK STT Adisutjipto Yogyakarta Teknika STTKD: : Jurnal Teknik, Elektronik, Engine
Arfie Armelia Erissonia
Sekolah Tinggi Teknologi Kedirgantaraan
Aerospace Engineering Computer Science & IT Electrical & Electronics Engineering Energy Industrial & Manufacturing Engineering Materials Science & Nanotechnology Mechanical Engineering

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Studi Parametrik pada Flapping-Wing MAV dengan Bentuk Sayap Belalang, Kupu-kupu dan Kumbang Reo Yudhono; Arfie Armelia Erissonia; Haris Ardianto
SENATIK STT Adisutjipto Vol 3 (2017): Dukungan Teknologi Untuk Pengembangan Industri Dirgantara Indonesia
Publisher : Institut Teknologi Dirgantara Adisutjipto

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.28989/senatik.v3i0.102

Abstract

Nature has been a great inspiration for engineering design. Flying insect, in specific, has been studied and being an inspiration in the development of flapping-wing micro aerial vehicle (FW-MAV). Each species of flying insect has its own wing kinematics, but most all of them generate the aerodynamic force with the same of three mechanism: delayed stall, rotational circulation and wake capture[1]. In this research, we conduct a parametric study on the FW-MAV with different wing shapes. There are two designs of the FW-MAV in this study, which have flapping angle of 80 and 120 deg. The three different shapes of wings are mimics from: desert locust, Monarch butterfly and rhinoceros beetle. The wings then attached to the FW-MAV and operated with voltage input of 1.5V. The force generated by the FW-MAV and the electrical current measured in a swing test, while recorded in 240 fps using action camera. From the test, we get the flapping frequency, generated horizontal force and power consumption. From this research we have several data that can be used for the further development of the FW-MAV.
PERANCANGAN SISTEM KENDALI MENIRU BURUNG UNTUK UNMMANED AERIAL VEHICLE BERKONFIGURASI SAYAP TETAP admin admin; Reo Yudhono; Arfie Armelia Erissonia
Teknika STTKD: : Jurnal Teknik, Elektronik, Engine Vol 5 No 2 (2018): Teknika STTKD: Jurnal Teknik, Elektronik, Engine
Publisher : Sekolah Tinggi Teknologi Kedirgantaraan

Show Abstract | Download Original | Original Source | Check in Google Scholar | Full PDF (631.881 KB)

Abstract

Bird is the main inspiration in the development of aircraft. The control mechanism on bird’s wing and tail, with simplification, has been applied to aircraft. Bird has simple yet advance control mechanism. Bird’s wing and tail have ability to morph its shape during the flight, in terms of stabilization and control. In this research, we design a control system mimicking bird control mechanism. Both the control surface and it’s mechanism is design mimicking the them on bird. The control surface on wings are the whole outer part of wing. While the tail can be rotate on 2 axis: longitudinal axis and it’s perpendicular axis. A simulation platform is made to shows how the designed control system’s works, which this control system will be installed to the bird-mimicking UAV airframe later. The components that used in the control system are: battery, autopilot (flight controller), servo, motor controller, motor and receiver. The designed control system has shown good respon to the given control command.
Co-Authors admin admin Haris Ardianto Reo Yudhono