Mostafa Rahimi Dizadji, A. Yousefi-Koma, Ziba Gharehnazifam
{"title":"基于自适应直接模糊控制器的卫星三轴姿态控制","authors":"Mostafa Rahimi Dizadji, A. Yousefi-Koma, Ziba Gharehnazifam","doi":"10.1109/ICROM.2018.8657560","DOIUrl":null,"url":null,"abstract":"The research is dedicated to design an adaptive direct fuzzy control system for a typical satellite to attain desired orientation. Satellite dynamic is obtained using Euler formulation. Having kinematics from quaternion description of the attitude control, the combined nonlinear model is provided. Sliding surface used as primary variable of the adaptive law to regulate the output of direct fuzzy controller. In order to evaluate the designed controller performance, different simulations are performed in the presence of disturbance. Comparing the simulation results against that of a typical classic controller shows the significant improvement in the system response.","PeriodicalId":383818,"journal":{"name":"2018 6th RSI International Conference on Robotics and Mechatronics (IcRoM)","volume":"153 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2018-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"7","resultStr":"{\"title\":\"3-Axis Attitude Control of Satellite using Adaptive Direct Fuzzy Controller\",\"authors\":\"Mostafa Rahimi Dizadji, A. Yousefi-Koma, Ziba Gharehnazifam\",\"doi\":\"10.1109/ICROM.2018.8657560\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"The research is dedicated to design an adaptive direct fuzzy control system for a typical satellite to attain desired orientation. Satellite dynamic is obtained using Euler formulation. Having kinematics from quaternion description of the attitude control, the combined nonlinear model is provided. Sliding surface used as primary variable of the adaptive law to regulate the output of direct fuzzy controller. In order to evaluate the designed controller performance, different simulations are performed in the presence of disturbance. Comparing the simulation results against that of a typical classic controller shows the significant improvement in the system response.\",\"PeriodicalId\":383818,\"journal\":{\"name\":\"2018 6th RSI International Conference on Robotics and Mechatronics (IcRoM)\",\"volume\":\"153 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2018-10-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"7\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2018 6th RSI International Conference on Robotics and Mechatronics (IcRoM)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/ICROM.2018.8657560\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2018 6th RSI International Conference on Robotics and Mechatronics (IcRoM)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICROM.2018.8657560","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
3-Axis Attitude Control of Satellite using Adaptive Direct Fuzzy Controller
The research is dedicated to design an adaptive direct fuzzy control system for a typical satellite to attain desired orientation. Satellite dynamic is obtained using Euler formulation. Having kinematics from quaternion description of the attitude control, the combined nonlinear model is provided. Sliding surface used as primary variable of the adaptive law to regulate the output of direct fuzzy controller. In order to evaluate the designed controller performance, different simulations are performed in the presence of disturbance. Comparing the simulation results against that of a typical classic controller shows the significant improvement in the system response.
求助内容：
应助结果提醒方式：
京公网安备 11010802042870号
