Evaluation of Optimized Inner and Outer Loop Controllers for 4X Flyer under Faulty Actuators
Metaheuristic optimization techniques are a powerful tool to decide the optimal gains for underactuated systems such as quadrotors, considering the multiple controllers involved in the inner and outer loops of the system. This paper deals with the evaluation of performance of the set of controllers...
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Veröffentlicht in: | Automatic control and computer sciences 2023-12, Vol.57 (6), p.563-576 |
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creator | Nasri Boualem Abderrezak, Guessoum Lotfi, Mostefai Bensikaddour El habib Nabil, Hamdadou Abdelhamid, Ghoul Akram, Adnane |
description | Metaheuristic optimization techniques are a powerful tool to decide the optimal gains for underactuated systems such as quadrotors, considering the multiple controllers involved in the inner and outer loops of the system. This paper deals with the evaluation of performance of the set of controllers (PI and SMC) set by three optimization methods: particle swarm optimization (PSO), grey wolf optimization (GWO), and equilibrium optimization (EO). The disparity of the control gains obtained during the optimization is a sign of the distinction between performance reached by each controller. The proposed study investigates this difference through a robustness test by gradually including faults to the quadrotor actuators. We observed degradation in the agility of quadrotor (stabilization of altitude and attitude) for the faulty case; however, the three controllers showed different tolerances to the fault. The simulation results show that the parameters optimized by EO algorithm, outperform both the PSO and the GWO algorithm, especially for the considered unfavorable cases. |
doi_str_mv | 10.3103/S0146411623060032 |
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This paper deals with the evaluation of performance of the set of controllers (PI and SMC) set by three optimization methods: particle swarm optimization (PSO), grey wolf optimization (GWO), and equilibrium optimization (EO). The disparity of the control gains obtained during the optimization is a sign of the distinction between performance reached by each controller. The proposed study investigates this difference through a robustness test by gradually including faults to the quadrotor actuators. We observed degradation in the agility of quadrotor (stabilization of altitude and attitude) for the faulty case; however, the three controllers showed different tolerances to the fault. 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Control Comp. Sci</addtitle><description>Metaheuristic optimization techniques are a powerful tool to decide the optimal gains for underactuated systems such as quadrotors, considering the multiple controllers involved in the inner and outer loops of the system. This paper deals with the evaluation of performance of the set of controllers (PI and SMC) set by three optimization methods: particle swarm optimization (PSO), grey wolf optimization (GWO), and equilibrium optimization (EO). The disparity of the control gains obtained during the optimization is a sign of the distinction between performance reached by each controller. The proposed study investigates this difference through a robustness test by gradually including faults to the quadrotor actuators. We observed degradation in the agility of quadrotor (stabilization of altitude and attitude) for the faulty case; however, the three controllers showed different tolerances to the fault. The simulation results show that the parameters optimized by EO algorithm, outperform both the PSO and the GWO algorithm, especially for the considered unfavorable cases.</description><subject>Actuators</subject><subject>Algorithms</subject><subject>Computer Science</subject><subject>Control Structures and Microprogramming</subject><subject>Controllers</subject><subject>Heuristic methods</subject><subject>Optimization techniques</subject><subject>Particle swarm optimization</subject><subject>Performance evaluation</subject><subject>Rotary wing aircraft</subject><subject>Tolerances</subject><issn>0146-4116</issn><issn>1558-108X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2023</creationdate><recordtype>article</recordtype><recordid>eNp1kE9LAzEQxYMoWKsfwFvA82r-bZI9ltJqodCDCj0IS7pJZMs2WZOssH56Uyp4EC8zw_zeewMDwC1G9xQj-vCMMOMMY04o4ghRcgYmuCxlgZHcnoPJERdHfgmuYtwjlJnkE_C2-FTdoFLrHfQWbvrUHtovo-HKOROgchpuhpSntfc9nHuXgu86EyK0PkC2hctuzHRwOtelGro0wlmTcqIP8RpcWNVFc_PTp-B1uXiZPxXrzeNqPlsXDeEyFcTIqlIlbnaMack1qTRmRAtMuMFCUSMZ10wYU5Wcobwr7Y4KagU3SNhK0Cm4O-X2wX8MJqZ674fg8smayIoxyksiswqfVE3wMQZj6z60BxXGGqP6-MT6zxOzh5w8MWvduwm_yf-bvgES4XJK</recordid><startdate>20231201</startdate><enddate>20231201</enddate><creator>Nasri Boualem</creator><creator>Abderrezak, Guessoum</creator><creator>Lotfi, Mostefai</creator><creator>Bensikaddour El habib</creator><creator>Nabil, Hamdadou</creator><creator>Abdelhamid, Ghoul</creator><creator>Akram, Adnane</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20231201</creationdate><title>Evaluation of Optimized Inner and Outer Loop Controllers for 4X Flyer under Faulty Actuators</title><author>Nasri Boualem ; Abderrezak, Guessoum ; Lotfi, Mostefai ; Bensikaddour El habib ; Nabil, Hamdadou ; Abdelhamid, Ghoul ; Akram, Adnane</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c268t-2e899a51cb44d86d29d142d7126e17a3e846d47ee956406e15fb373f76e07f973</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2023</creationdate><topic>Actuators</topic><topic>Algorithms</topic><topic>Computer Science</topic><topic>Control Structures and Microprogramming</topic><topic>Controllers</topic><topic>Heuristic methods</topic><topic>Optimization techniques</topic><topic>Particle swarm optimization</topic><topic>Performance evaluation</topic><topic>Rotary wing aircraft</topic><topic>Tolerances</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Nasri Boualem</creatorcontrib><creatorcontrib>Abderrezak, Guessoum</creatorcontrib><creatorcontrib>Lotfi, Mostefai</creatorcontrib><creatorcontrib>Bensikaddour El habib</creatorcontrib><creatorcontrib>Nabil, Hamdadou</creatorcontrib><creatorcontrib>Abdelhamid, Ghoul</creatorcontrib><creatorcontrib>Akram, Adnane</creatorcontrib><collection>CrossRef</collection><jtitle>Automatic control and computer sciences</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Nasri Boualem</au><au>Abderrezak, Guessoum</au><au>Lotfi, Mostefai</au><au>Bensikaddour El habib</au><au>Nabil, Hamdadou</au><au>Abdelhamid, Ghoul</au><au>Akram, Adnane</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Evaluation of Optimized Inner and Outer Loop Controllers for 4X Flyer under Faulty Actuators</atitle><jtitle>Automatic control and computer sciences</jtitle><stitle>Aut. 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We observed degradation in the agility of quadrotor (stabilization of altitude and attitude) for the faulty case; however, the three controllers showed different tolerances to the fault. The simulation results show that the parameters optimized by EO algorithm, outperform both the PSO and the GWO algorithm, especially for the considered unfavorable cases.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.3103/S0146411623060032</doi><tpages>14</tpages></addata></record> |
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subjects | Actuators Algorithms Computer Science Control Structures and Microprogramming Controllers Heuristic methods Optimization techniques Particle swarm optimization Performance evaluation Rotary wing aircraft Tolerances |
title | Evaluation of Optimized Inner and Outer Loop Controllers for 4X Flyer under Faulty Actuators |
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