{"title":"Synthesizing an Adaptive Controller to Enhance Movement Quality of a Flight Control Actuator under External Load","authors":"Dinh Khanh Nguyen, V. Kuznetsov, Cao Nhu Vung","doi":"10.1109/CTS53513.2021.9562850","DOIUrl":null,"url":null,"abstract":"The article provides a study into highperformance, efficient and reliable adaptive motion control over an electro-hydraulic actuator (EHA) considering external load disturbance impacting the system. The article considers the dynamics of an electro-hydraulic system taking into account servo-valve flow-pressure curves. In addition to the non-linear nature of hydraulic dynamics, an electro-hydraulic flight control actuator system is defined by the limited uncertainty of model description and is subject to external load disturbance. The synthesis of an adaptive system, which ensures a higher quality movement of a flight control actuator under external load, is carried out by the method of Lyapunov functions. The research was carried out in the MATLAB/ Simulink software environment.","PeriodicalId":371882,"journal":{"name":"2021 IV International Conference on Control in Technical Systems (CTS)","volume":"41 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2021-09-21","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2021 IV International Conference on Control in Technical Systems (CTS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CTS53513.2021.9562850","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
The article provides a study into highperformance, efficient and reliable adaptive motion control over an electro-hydraulic actuator (EHA) considering external load disturbance impacting the system. The article considers the dynamics of an electro-hydraulic system taking into account servo-valve flow-pressure curves. In addition to the non-linear nature of hydraulic dynamics, an electro-hydraulic flight control actuator system is defined by the limited uncertainty of model description and is subject to external load disturbance. The synthesis of an adaptive system, which ensures a higher quality movement of a flight control actuator under external load, is carried out by the method of Lyapunov functions. The research was carried out in the MATLAB/ Simulink software environment.