Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin

Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin

The flight quality or behaviour of a blended-wing-body (BWB) unmanned aerial system (UAS) could be gathered and evaluated through virtual simulation or software-in-theloop (SITL) simulation. This is done through a specific setup between a ground control station (GCS) software, Mission Planner and...

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Bibliographic Details
Main Author: Zainurin, Shahrean
Format: Thesis
Language:English
Published: 2020
Subjects:
Computer simulation
Online Access:https://ir.uitm.edu.my/id/eprint/60049/1/60049.pdf
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spelling my-uitm-ir.600492022-05-21T01:08:49Z Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin 2020-08 Zainurin, Shahrean Computer simulation The flight quality or behaviour of a blended-wing-body (BWB) unmanned aerial system (UAS) could be gathered and evaluated through virtual simulation or software-in-theloop (SITL) simulation. This is done through a specific setup between a ground control station (GCS) software, Mission Planner and a flight simulation software, X-Plane 11. BWB UAS flight dynamics, unlike conventional aircraft, can be unstable or have poor flying quality. Performing real flight testing can be very costly in the long run. The best solution to counter these drawbacks is to simulate flying behaviour virtually, before the first prototype is developed and before actual flight test is conducted. A specific and suitable simulation and testing is chosen to determine and improve the flight dynamics and behaviour of the BWB aircraft. Throughout this experiment, Baseline-IX BWB UAS, developed by Flight Technology & Test Center, Universiti Teknologi MARA (UiTM) was used as the model in the simulation software, which also provides the environment model, for example, wind, turbulence, time of day. A flight simulation was configured as per real flight and connected to the simulation computer, rather than the physical UAS. 2020-08 Thesis https://ir.uitm.edu.my/id/eprint/60049/ https://ir.uitm.edu.my/id/eprint/60049/1/60049.pdf text en public masters Universiti Teknologi MARA Faculty of Mechanical Engineering M. Nasir, Rizal Effendy (Dr.)
institution Universiti Teknologi MARA
collection UiTM Institutional Repository
language English
advisor M. Nasir, Rizal Effendy (Dr.)
topic Computer simulation
spellingShingle Computer simulation
Zainurin, Shahrean
Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin
description The flight quality or behaviour of a blended-wing-body (BWB) unmanned aerial system (UAS) could be gathered and evaluated through virtual simulation or software-in-theloop (SITL) simulation. This is done through a specific setup between a ground control station (GCS) software, Mission Planner and a flight simulation software, X-Plane 11. BWB UAS flight dynamics, unlike conventional aircraft, can be unstable or have poor flying quality. Performing real flight testing can be very costly in the long run. The best solution to counter these drawbacks is to simulate flying behaviour virtually, before the first prototype is developed and before actual flight test is conducted. A specific and suitable simulation and testing is chosen to determine and improve the flight dynamics and behaviour of the BWB aircraft. Throughout this experiment, Baseline-IX BWB UAS, developed by Flight Technology & Test Center, Universiti Teknologi MARA (UiTM) was used as the model in the simulation software, which also provides the environment model, for example, wind, turbulence, time of day. A flight simulation was configured as per real flight and connected to the simulation computer, rather than the physical UAS.
format Thesis
qualification_level Master's degree
author Zainurin, Shahrean
author_facet Zainurin, Shahrean
author_sort Zainurin, Shahrean
title Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin
title_short Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin
title_full Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin
title_fullStr Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin
title_full_unstemmed Flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / Shahrean Zainurin
title_sort flight dynamic stability performance of the baseline-ix blended-wing-body unmanned aerial system using flight simulator / shahrean zainurin
granting_institution Universiti Teknologi MARA
granting_department Faculty of Mechanical Engineering
publishDate 2020
url https://ir.uitm.edu.my/id/eprint/60049/1/60049.pdf
_version_ 1783735075847798784

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