ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE

ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE

MiniBe is an UAV (Unmanned Aerial Vehicle) that is a flying wing aircraft. A flying wing only has one type of control surface that is elevon. Elevon is a combination of elevator and aileron. This research started with developing a proper MiniBe UAV to an aircraft model that can be flown with X-Pl...

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Main Author: Nuril Fahmi, Muhammad
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/62649
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:62649
spelling id-itb.:626492022-01-17T09:19:32ZESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE Nuril Fahmi, Muhammad Indonesia Final Project UAV, X-Plane, aerodynamic coefficients, stability coefficients INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/62649 MiniBe is an UAV (Unmanned Aerial Vehicle) that is a flying wing aircraft. A flying wing only has one type of control surface that is elevon. Elevon is a combination of elevator and aileron. This research started with developing a proper MiniBe UAV to an aircraft model that can be flown with X-Plane software. The purposes of this research are to develop flight test method on a simulation program and find out X-Plane ability in estimating aerodynamics and stability coefficient. Aerodynamic and stability coefficient derivatives are calculated based on linear coefficient equation model that is solved by multi parameter linear regression. The result of the coefficients will be compared with DATCOM estimation to evaluate X-Plane simulation performance. The result of the coefficient comparison analysis will leads to recommendations so that the next research will obtain a better result. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description MiniBe is an UAV (Unmanned Aerial Vehicle) that is a flying wing aircraft. A flying wing only has one type of control surface that is elevon. Elevon is a combination of elevator and aileron. This research started with developing a proper MiniBe UAV to an aircraft model that can be flown with X-Plane software. The purposes of this research are to develop flight test method on a simulation program and find out X-Plane ability in estimating aerodynamics and stability coefficient. Aerodynamic and stability coefficient derivatives are calculated based on linear coefficient equation model that is solved by multi parameter linear regression. The result of the coefficients will be compared with DATCOM estimation to evaluate X-Plane simulation performance. The result of the coefficient comparison analysis will leads to recommendations so that the next research will obtain a better result.
format Final Project
author Nuril Fahmi, Muhammad
spellingShingle Nuril Fahmi, Muhammad
ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE
author_facet Nuril Fahmi, Muhammad
author_sort Nuril Fahmi, Muhammad
title ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE
title_short ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE
title_full ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE
title_fullStr ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE
title_full_unstemmed ESTIMASI KOEFISIEN AERODINAMIKA DAN TURUNAN KESTABILAN UAV FIXED-WING MENGGUNAKAN X-PLANE
title_sort estimasi koefisien aerodinamika dan turunan kestabilan uav fixed-wing menggunakan x-plane
url https://digilib.itb.ac.id/gdl/view/62649
_version_ 1822004138767024128

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