New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV

Currently, fuzzy proportional integral derivative (PID) controller schemes, which include simplified fuzzy reasoning decision methodologies and PID parameters, are broadly and efficaciously practiced in various fields from industrial applications, military service, to rescue operations, civilian inf...

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Main Authors: Huu Khoa Tran, Juing-Shian Chiou, Viet-Hung Dang
Format: Article
Language:English
Published: MDPI AG 2020-09-01
Series:Mathematics
Subjects:
Online Access:https://www.mdpi.com/2227-7390/8/9/1499
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spelling doaj-e9a2aed7a72b4bc9a22d7297c2c979482020-11-25T03:20:45ZengMDPI AGMathematics2227-73902020-09-0181499149910.3390/math8091499New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAVHuu Khoa Tran0Juing-Shian Chiou1Viet-Hung Dang2Center for Cyber-Physical System Innovation, National Taiwan University of Science and Technology, Taipei 10607, TaiwanDepartment of Electrical Engineering, Southern Taiwan University of Science and Technology, Tainan 71005, TaiwanFaculty of Information Technology, Duy Tan University, Danang 50000, VietnamCurrently, fuzzy proportional integral derivative (PID) controller schemes, which include simplified fuzzy reasoning decision methodologies and PID parameters, are broadly and efficaciously practiced in various fields from industrial applications, military service, to rescue operations, civilian information and also horticultural observation and agricultural surveillance. A fusion particle swarm optimization (PSO)–evolutionary programming (EP) algorithm, which is an improved version of the stochastic optimization strategy PSO, was presented for designing and optimizing controller gains in this study. The mathematical calculations of this study include the reproduction of EP with PSO. By minimizing the integral of the absolute error (IAE) criterion that is used for estimating the system response as a fitness function, the obtained integrated design of the fusion PSO–EP algorithm generated and updated the new elite parameters for proposed controller schemes. This progression was used for the complicated non-linear systems of the attitude-control pilot models of a tricopter unmanned aerial vehicle (UAV) to demonstrate an improvement on the performance in terms of rapid response, precision, reliability, and stability.https://www.mdpi.com/2227-7390/8/9/1499particle swarm optimization (PSO)evolutionary programming (EP)fuzzy controlproportional–integral–derivative controllerintegral of absolute error (IAE) criterionattitude control
collection DOAJ
language English
format Article
sources DOAJ
author Huu Khoa Tran
Juing-Shian Chiou
Viet-Hung Dang
spellingShingle Huu Khoa Tran
Juing-Shian Chiou
Viet-Hung Dang
New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV
Mathematics
particle swarm optimization (PSO)
evolutionary programming (EP)
fuzzy control
proportional–integral–derivative controller
integral of absolute error (IAE) criterion
attitude control
author_facet Huu Khoa Tran
Juing-Shian Chiou
Viet-Hung Dang
author_sort Huu Khoa Tran
title New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV
title_short New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV
title_full New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV
title_fullStr New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV
title_full_unstemmed New Fusion Algorithm-Reinforced Pilot Control for an Agricultural Tricopter UAV
title_sort new fusion algorithm-reinforced pilot control for an agricultural tricopter uav
publisher MDPI AG
series Mathematics
issn 2227-7390
publishDate 2020-09-01
description Currently, fuzzy proportional integral derivative (PID) controller schemes, which include simplified fuzzy reasoning decision methodologies and PID parameters, are broadly and efficaciously practiced in various fields from industrial applications, military service, to rescue operations, civilian information and also horticultural observation and agricultural surveillance. A fusion particle swarm optimization (PSO)–evolutionary programming (EP) algorithm, which is an improved version of the stochastic optimization strategy PSO, was presented for designing and optimizing controller gains in this study. The mathematical calculations of this study include the reproduction of EP with PSO. By minimizing the integral of the absolute error (IAE) criterion that is used for estimating the system response as a fitness function, the obtained integrated design of the fusion PSO–EP algorithm generated and updated the new elite parameters for proposed controller schemes. This progression was used for the complicated non-linear systems of the attitude-control pilot models of a tricopter unmanned aerial vehicle (UAV) to demonstrate an improvement on the performance in terms of rapid response, precision, reliability, and stability.
topic particle swarm optimization (PSO)
evolutionary programming (EP)
fuzzy control
proportional–integral–derivative controller
integral of absolute error (IAE) criterion
attitude control
url https://www.mdpi.com/2227-7390/8/9/1499
work_keys_str_mv AT huukhoatran newfusionalgorithmreinforcedpilotcontrolforanagriculturaltricopteruav
AT juingshianchiou newfusionalgorithmreinforcedpilotcontrolforanagriculturaltricopteruav
AT viethungdang newfusionalgorithmreinforcedpilotcontrolforanagriculturaltricopteruav
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