Autonomous formation flight control of multiple UAVs with motion capture system

The evolution from a single entity to multiple entity flight has introduced numerous possibilities of performing multi task by using multiple agent system. In a multiple entity flight or formation, the search in a feasible way of acquiring individual position and attitude estimation system as a dece...

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Main Author: M. F., Abas
Format: Thesis
Language:English
Published: 2013
Subjects:
Online Access:http://umpir.ump.edu.my/id/eprint/7643/
http://umpir.ump.edu.my/id/eprint/7643/
http://umpir.ump.edu.my/id/eprint/7643/1/MOHAMMAD_FADHIL_BIN_ABAS.PDF
id ump-7643
recordtype eprints
spelling ump-76432017-10-17T07:38:47Z http://umpir.ump.edu.my/id/eprint/7643/ Autonomous formation flight control of multiple UAVs with motion capture system M. F., Abas TL Motor vehicles. Aeronautics. Astronautics The evolution from a single entity to multiple entity flight has introduced numerous possibilities of performing multi task by using multiple agent system. In a multiple entity flight or formation, the search in a feasible way of acquiring individual position and attitude estimation system as a decentralized system has include the use of GPS, INS, Onboard Stereo Camera, Laser Range Finder and also Motion Capture System. The feasibility of each method of position and attitude estimation system as a decentralized system is presented as a part of this thesis. The use of onboard stereo camera is very promising for decentralized system but at the current state of onboard technology, the speed of the onboard stereo camera system is very slow. GPS in the other hand is widely used but the accuracy of such system for short range formation flight is questionable. For formation flight testing and evaluation, the used of motion capture system is very reliable. Formation flight for multiple agents Quad-rotor Aerial Vehicles (QAVs) has lead from conventional way of leader-follower formation flight to nature based formation flight. The first part of the formation in this thesis is based on a conventional way of leader-follower formation. The formation developed is a Simultaneous Angle and Distance Regulation (SADR). This type of formation is used for a curving or circular motion where by the distance of the leader-follower through the center and the angle between the leader and follower is regulated. Although the development has yielded good result, some negative attributes can be seen. The first is that the whole system relies directly on the leader. If the leader were nonfunctional, the whole system will be nonfunctional. There is no policy of algorithm were by the leader's task can be pass to other quad-rotor UAV. 2013 Thesis NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/7643/1/MOHAMMAD_FADHIL_BIN_ABAS.PDF M. F., Abas (2013) Autonomous formation flight control of multiple UAVs with motion capture system. PhD thesis, Chiba, Japan : Chiba University. http://iportal.ump.edu.my/lib/item?id=chamo:75680&theme=UMP2
repository_type Digital Repository
institution_category Local University
institution Universiti Malaysia Pahang
building UMP Institutional Repository
collection Online Access
language English
topic TL Motor vehicles. Aeronautics. Astronautics
spellingShingle TL Motor vehicles. Aeronautics. Astronautics
M. F., Abas
Autonomous formation flight control of multiple UAVs with motion capture system
description The evolution from a single entity to multiple entity flight has introduced numerous possibilities of performing multi task by using multiple agent system. In a multiple entity flight or formation, the search in a feasible way of acquiring individual position and attitude estimation system as a decentralized system has include the use of GPS, INS, Onboard Stereo Camera, Laser Range Finder and also Motion Capture System. The feasibility of each method of position and attitude estimation system as a decentralized system is presented as a part of this thesis. The use of onboard stereo camera is very promising for decentralized system but at the current state of onboard technology, the speed of the onboard stereo camera system is very slow. GPS in the other hand is widely used but the accuracy of such system for short range formation flight is questionable. For formation flight testing and evaluation, the used of motion capture system is very reliable. Formation flight for multiple agents Quad-rotor Aerial Vehicles (QAVs) has lead from conventional way of leader-follower formation flight to nature based formation flight. The first part of the formation in this thesis is based on a conventional way of leader-follower formation. The formation developed is a Simultaneous Angle and Distance Regulation (SADR). This type of formation is used for a curving or circular motion where by the distance of the leader-follower through the center and the angle between the leader and follower is regulated. Although the development has yielded good result, some negative attributes can be seen. The first is that the whole system relies directly on the leader. If the leader were nonfunctional, the whole system will be nonfunctional. There is no policy of algorithm were by the leader's task can be pass to other quad-rotor UAV.
format Thesis
author M. F., Abas
author_facet M. F., Abas
author_sort M. F., Abas
title Autonomous formation flight control of multiple UAVs with motion capture system
title_short Autonomous formation flight control of multiple UAVs with motion capture system
title_full Autonomous formation flight control of multiple UAVs with motion capture system
title_fullStr Autonomous formation flight control of multiple UAVs with motion capture system
title_full_unstemmed Autonomous formation flight control of multiple UAVs with motion capture system
title_sort autonomous formation flight control of multiple uavs with motion capture system
publishDate 2013
url http://umpir.ump.edu.my/id/eprint/7643/
http://umpir.ump.edu.my/id/eprint/7643/
http://umpir.ump.edu.my/id/eprint/7643/1/MOHAMMAD_FADHIL_BIN_ABAS.PDF
first_indexed 2023-09-18T22:04:27Z
last_indexed 2023-09-18T22:04:27Z
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