{"title":"THE MATHEMATICAL AND SIMULINK MODELS FOR DETERMINING ATTITUDE OF AIRCRAFT USING MEMS SENSORS","authors":"I. Isgandarov, H.E. Bakhshiyev","doi":"10.53364/24138614_2022_25_2_8","DOIUrl":null,"url":null,"abstract":"","PeriodicalId":341139,"journal":{"name":"Вестник Академии гражданской авиации","volume":"35 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Вестник Академии гражданской авиации","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.53364/24138614_2022_25_2_8","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}