{"title":"High Precision Loading Control Method for Sun-Tracking Unit Semi-physical Test System","authors":"Mingyang Liu, Zhigang Xu, Zhen Zhao, Xinlin Bai, Yueling Chen","doi":"10.1109/ICCA.2019.8899599","DOIUrl":null,"url":null,"abstract":"in this paper, a semi-physical ground test technology is proposed to simulate the disturbance of flexible solar panels on sun-tracking unit. In order to improve the precision of the semi-physical test, several methods have been designed. Firstly, semi-physical test platform with ultra-high stiffness and automatically adapted to motion errors without additional force is designed to provide foundation. Secondly, solar wing dynamic model is established and discrete by Wilson 6 method to calculate torque by real-time system. Thirdly, angular acceleration estimation of sun-tracking unit is obtained by nonlinear tracking-differentiator. Finally, simulation and experiment results show that platform can provide disturbance simulation torque, the platform can test the performance of sun-tracking unit.","PeriodicalId":130891,"journal":{"name":"2019 IEEE 15th International Conference on Control and Automation (ICCA)","volume":"81 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-07-16","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 IEEE 15th International Conference on Control and Automation (ICCA)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICCA.2019.8899599","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0
Abstract
in this paper, a semi-physical ground test technology is proposed to simulate the disturbance of flexible solar panels on sun-tracking unit. In order to improve the precision of the semi-physical test, several methods have been designed. Firstly, semi-physical test platform with ultra-high stiffness and automatically adapted to motion errors without additional force is designed to provide foundation. Secondly, solar wing dynamic model is established and discrete by Wilson 6 method to calculate torque by real-time system. Thirdly, angular acceleration estimation of sun-tracking unit is obtained by nonlinear tracking-differentiator. Finally, simulation and experiment results show that platform can provide disturbance simulation torque, the platform can test the performance of sun-tracking unit.