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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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 |
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