Development of load carrying and releasing system of hexacopter

An unmanned aerial vehicle (UAV) which is integrated with the gripper system is be able to provide diverse service to the society. The objective of this project is to develop a load carrying and releasing system for hexacopter platform. The proposed method is to use the hexacopter with high payload...

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Main Authors:	Zakaria, Abdul Hafiz, Mohd Mustafah, Yasir, Mohd. Hatta, Muhd. Mudzakkir, N. Azlan, Muhd Nadzif
Format:	Conference or Workshop Item
Language:	English English English
Published:	IEEE 2015
Subjects:	T Technology (General)
Online Access:	http://irep.iium.edu.my/49426/ http://irep.iium.edu.my/49426/ http://irep.iium.edu.my/49426/ http://irep.iium.edu.my/49426/4/49426_development_of_load_carrying_scopus.pdf http://irep.iium.edu.my/49426/9/49426-Development_of_load_carrying_and_releasing_system_of_hexacopter_Fullpaper.pdf http://irep.iium.edu.my/49426/12/ASCC-organizer.pdf

id	iium-49426
recordtype	eprints
spelling	iium-494262016-05-24T04:06:16Z http://irep.iium.edu.my/49426/ Development of load carrying and releasing system of hexacopter Zakaria, Abdul Hafiz Mohd Mustafah, Yasir Mohd. Hatta, Muhd. Mudzakkir N. Azlan, Muhd Nadzif T Technology (General) An unmanned aerial vehicle (UAV) which is integrated with the gripper system is be able to provide diverse service to the society. The objective of this project is to develop a load carrying and releasing system for hexacopter platform. The proposed method is to use the hexacopter with high payload capable of flying while carrying some extra load. A gripper system with the ability to hold and release the preloaded object is designed to enable the hexacopter to transport objects. The load carrying and releasing system releases the object after receiving an instruction from the user. During the flight, mission planner is used to monitor the flight status. The hexacopter performance was evaluated through a series of flight tests. The result from the experiments show that the total flight time of the hexacopter reduced by 5 minutes from the normal time of 15 minutes when the load carrying mechanism is attached. This is because attaching the mechanism increases the total payload by 800grams from the normal payload of 2.2kg. Payload increment means higher current drawn from the battery to produce higher motor speed. Attaching the mechanism also affects the stabilization of the UAV. Hence, retuning of the PID controller was performed in order to correct the flight attitude of the UAV. This project successfully demonstrated the development of load carrying and releasing system which might serve as guidelines for other related future projects. IEEE 2015 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/49426/4/49426_development_of_load_carrying_scopus.pdf application/pdf en http://irep.iium.edu.my/49426/9/49426-Development_of_load_carrying_and_releasing_system_of_hexacopter_Fullpaper.pdf application/pdf en http://irep.iium.edu.my/49426/12/ASCC-organizer.pdf Zakaria, Abdul Hafiz and Mohd Mustafah, Yasir and Mohd. Hatta, Muhd. Mudzakkir and N. Azlan, Muhd Nadzif (2015) Development of load carrying and releasing system of hexacopter. In: 2015 10th Asian Control Conference (ASCC 2015), 31st May- 3rd June 2015, Kota Kinabalu, Sabah. http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=7244701&tag=1 10.1109/ASCC.2015.7244701
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English English
topic	T Technology (General)
spellingShingle	T Technology (General) Zakaria, Abdul Hafiz Mohd Mustafah, Yasir Mohd. Hatta, Muhd. Mudzakkir N. Azlan, Muhd Nadzif Development of load carrying and releasing system of hexacopter
description	An unmanned aerial vehicle (UAV) which is integrated with the gripper system is be able to provide diverse service to the society. The objective of this project is to develop a load carrying and releasing system for hexacopter platform. The proposed method is to use the hexacopter with high payload capable of flying while carrying some extra load. A gripper system with the ability to hold and release the preloaded object is designed to enable the hexacopter to transport objects. The load carrying and releasing system releases the object after receiving an instruction from the user. During the flight, mission planner is used to monitor the flight status. The hexacopter performance was evaluated through a series of flight tests. The result from the experiments show that the total flight time of the hexacopter reduced by 5 minutes from the normal time of 15 minutes when the load carrying mechanism is attached. This is because attaching the mechanism increases the total payload by 800grams from the normal payload of 2.2kg. Payload increment means higher current drawn from the battery to produce higher motor speed. Attaching the mechanism also affects the stabilization of the UAV. Hence, retuning of the PID controller was performed in order to correct the flight attitude of the UAV. This project successfully demonstrated the development of load carrying and releasing system which might serve as guidelines for other related future projects.
format	Conference or Workshop Item
author	Zakaria, Abdul Hafiz Mohd Mustafah, Yasir Mohd. Hatta, Muhd. Mudzakkir N. Azlan, Muhd Nadzif
author_facet	Zakaria, Abdul Hafiz Mohd Mustafah, Yasir Mohd. Hatta, Muhd. Mudzakkir N. Azlan, Muhd Nadzif
author_sort	Zakaria, Abdul Hafiz
title	Development of load carrying and releasing system of hexacopter
title_short	Development of load carrying and releasing system of hexacopter
title_full	Development of load carrying and releasing system of hexacopter
title_fullStr	Development of load carrying and releasing system of hexacopter
title_full_unstemmed	Development of load carrying and releasing system of hexacopter
title_sort	development of load carrying and releasing system of hexacopter
publisher	IEEE
publishDate	2015
url	http://irep.iium.edu.my/49426/ http://irep.iium.edu.my/49426/ http://irep.iium.edu.my/49426/ http://irep.iium.edu.my/49426/4/49426_development_of_load_carrying_scopus.pdf http://irep.iium.edu.my/49426/9/49426-Development_of_load_carrying_and_releasing_system_of_hexacopter_Fullpaper.pdf http://irep.iium.edu.my/49426/12/ASCC-organizer.pdf
first_indexed	2023-09-18T21:09:53Z
last_indexed	2023-09-18T21:09:53Z
_version_	1777411181726662656

Development of load carrying and releasing system of hexacopter

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