A. Nebylov, Vladimir Nebylov, A. Panferov, S. Brodsky
{"title":"地效领域运动控制算法综合方法","authors":"A. Nebylov, Vladimir Nebylov, A. Panferov, S. Brodsky","doi":"10.23919/ICINS.2019.8769414","DOIUrl":null,"url":null,"abstract":"Methods for obtaining a software model of a winged aircraft (wind-in- ground effect vehicle) near a flat surface using the Comsol Multiphysics CFD package are considered. The scope of the resulting model was determined. A method for controlling an ekranoplane in a wide range of ground effect is proposed. The results of digital modeling are given.","PeriodicalId":108493,"journal":{"name":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","volume":"8 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Methods of Motion Control Algorithms Synthesis in the Area of Ground-Effect\",\"authors\":\"A. Nebylov, Vladimir Nebylov, A. Panferov, S. Brodsky\",\"doi\":\"10.23919/ICINS.2019.8769414\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Methods for obtaining a software model of a winged aircraft (wind-in- ground effect vehicle) near a flat surface using the Comsol Multiphysics CFD package are considered. The scope of the resulting model was determined. A method for controlling an ekranoplane in a wide range of ground effect is proposed. The results of digital modeling are given.\",\"PeriodicalId\":108493,\"journal\":{\"name\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"volume\":\"8 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2019-05-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ICINS.2019.8769414\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 26th Saint Petersburg International Conference on Integrated Navigation Systems (ICINS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ICINS.2019.8769414","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Methods of Motion Control Algorithms Synthesis in the Area of Ground-Effect
Methods for obtaining a software model of a winged aircraft (wind-in- ground effect vehicle) near a flat surface using the Comsol Multiphysics CFD package are considered. The scope of the resulting model was determined. A method for controlling an ekranoplane in a wide range of ground effect is proposed. The results of digital modeling are given.