{"title":"综合自适应控制器提高飞行控制作动器在外部负载下的运动质量","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":"{\"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}","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}
Synthesizing an Adaptive Controller to Enhance Movement Quality of a Flight Control Actuator under External Load
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.