Dynamic Stability of Aerostat-Drone

The current generation of drone lack extended hovering and flight capabilities. Equipping a drone with an inflatable structure such as aerostat can enhances endurance as aerostat can enhance the flight duration of the drone by using the buoyant force from gas. However, adding the aerostat to the...

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Main Author: Md Said, Mohd Shahruddin
Format: Final Year Project
Language: English
Institution: Universiti Teknologi Petronas
Record Id / ISBN-0: utp-utpedia.22624 /
Published: Universiti Teknologi PETRONAS 2016
Subjects:
TK Electrical engineering. Electronics Nuclear engineering
Online Access: http://utpedia.utp.edu.my/22624/1/Mohd%20Shahruddin%20bin%20Md%20Said%20-Dissertation.pdf
http://utpedia.utp.edu.my/22624/
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spelling utp-utpedia.226242022-02-17T07:57:02Z http://utpedia.utp.edu.my/22624/ Dynamic Stability of Aerostat-Drone Md Said, Mohd Shahruddin TK Electrical engineering. Electronics Nuclear engineering The current generation of drone lack extended hovering and flight capabilities. Equipping a drone with an inflatable structure such as aerostat can enhances endurance as aerostat can enhance the flight duration of the drone by using the buoyant force from gas. However, adding the aerostat to the drone can affect the stability of the drone and lead to less control performance of the drone. In this project, an experiment was conducted to test the effect of the aerostat on the drone stability in term of pitch, roll and yaw rate. A Simulink Dynamic Model of Aerostat-UAV from the previous project is simulated using MATLAB to compare with the actual dynamic behavior of the drone. Parrot AR.Drone, a quadcopter equipped with six sensors was used to collect the flight data. Universiti Teknologi PETRONAS 2016-09 Final Year Project NonPeerReviewed application/pdf en http://utpedia.utp.edu.my/22624/1/Mohd%20Shahruddin%20bin%20Md%20Said%20-Dissertation.pdf Md Said, Mohd Shahruddin (2016) Dynamic Stability of Aerostat-Drone. Universiti Teknologi PETRONAS. (Submitted)
institution Universiti Teknologi Petronas
collection UTPedia
language English
topic TK Electrical engineering. Electronics Nuclear engineering
spellingShingle TK Electrical engineering. Electronics Nuclear engineering
Md Said, Mohd Shahruddin
Dynamic Stability of Aerostat-Drone
description The current generation of drone lack extended hovering and flight capabilities. Equipping a drone with an inflatable structure such as aerostat can enhances endurance as aerostat can enhance the flight duration of the drone by using the buoyant force from gas. However, adding the aerostat to the drone can affect the stability of the drone and lead to less control performance of the drone. In this project, an experiment was conducted to test the effect of the aerostat on the drone stability in term of pitch, roll and yaw rate. A Simulink Dynamic Model of Aerostat-UAV from the previous project is simulated using MATLAB to compare with the actual dynamic behavior of the drone. Parrot AR.Drone, a quadcopter equipped with six sensors was used to collect the flight data.
format Final Year Project
author Md Said, Mohd Shahruddin
author_sort Md Said, Mohd Shahruddin
title Dynamic Stability of Aerostat-Drone
title_short Dynamic Stability of Aerostat-Drone
title_full Dynamic Stability of Aerostat-Drone
title_fullStr Dynamic Stability of Aerostat-Drone
title_full_unstemmed Dynamic Stability of Aerostat-Drone
title_sort dynamic stability of aerostat-drone
publisher Universiti Teknologi PETRONAS
publishDate 2016
url http://utpedia.utp.edu.my/22624/1/Mohd%20Shahruddin%20bin%20Md%20Said%20-Dissertation.pdf
http://utpedia.utp.edu.my/22624/
_version_ 1741195842806611968
score 11.62408

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