{"title":"Control simulation and anti-jamming verification of quadrotor UAV Based on Matlab","authors":"Zheyi Chen, Bing Xu","doi":"10.1109/ICIIBMS50712.2020.9336427","DOIUrl":null,"url":null,"abstract":"In this paper, the structure and the dynamic characteristics of quadrotor UAV are analyzed and studied in detail where the dynamic model of quadrotor UAV is established. The dynamic model is used to describe the flight attitude of quadrotor UAV, and the modeling of quadrotor UAV is carried out on the basis of the above mentioned information. Dynamic modeling is a simulation model established by the flight principle of the aircraft with the force relationship under various motion states such as referring to Newton Euler model. After the model is built, the simulation is carried out in Matlab / Simulink software to prove the merit of the method used.","PeriodicalId":243033,"journal":{"name":"2020 5th International Conference on Intelligent Informatics and Biomedical Sciences (ICIIBMS)","volume":"11 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-11-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 5th International Conference on Intelligent Informatics and Biomedical Sciences (ICIIBMS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICIIBMS50712.2020.9336427","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 1
Abstract
In this paper, the structure and the dynamic characteristics of quadrotor UAV are analyzed and studied in detail where the dynamic model of quadrotor UAV is established. The dynamic model is used to describe the flight attitude of quadrotor UAV, and the modeling of quadrotor UAV is carried out on the basis of the above mentioned information. Dynamic modeling is a simulation model established by the flight principle of the aircraft with the force relationship under various motion states such as referring to Newton Euler model. After the model is built, the simulation is carried out in Matlab / Simulink software to prove the merit of the method used.
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