{"title":"Error model of triaxial angular velocity sensor","authors":"D. Megyesi, R. Bréda, M. Matis","doi":"10.1109/NTAD.2019.8875566","DOIUrl":null,"url":null,"abstract":"The paper deals with the analysis of triaxial angular velocity sensor installed in IMU MNAV10CA. Sensor analysis is used to create a sensor model that includes sensor errors in individual axes as well as errors caused by a three-axis sensor design as a non-orthogonal error or misalignment. The authors of the article discuss the sequence of creating an error model, thanks to which it is possible to analyze interfering components in a useful sensor signal. The created model can then be used in the overall model of a small unmanned aircraft to increase its stability and controllability. Allan variation will be used to analyze the sensor noise processes.","PeriodicalId":186247,"journal":{"name":"2019 New Trends in Aviation Development (NTAD)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2019-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2019 New Trends in Aviation Development (NTAD)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/NTAD.2019.8875566","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
The paper deals with the analysis of triaxial angular velocity sensor installed in IMU MNAV10CA. Sensor analysis is used to create a sensor model that includes sensor errors in individual axes as well as errors caused by a three-axis sensor design as a non-orthogonal error or misalignment. The authors of the article discuss the sequence of creating an error model, thanks to which it is possible to analyze interfering components in a useful sensor signal. The created model can then be used in the overall model of a small unmanned aircraft to increase its stability and controllability. Allan variation will be used to analyze the sensor noise processes.