F. Guerrero, V. Martinez, O. García, D. Martinez-Vazquez
{"title":"Mini airplane: Design, aerodynamic modeling and stability","authors":"F. Guerrero, V. Martinez, O. García, D. Martinez-Vazquez","doi":"10.1109/ICEEE.2014.6978297","DOIUrl":null,"url":null,"abstract":"This paper presents the development of a mini airplane UAV, focusing on the aerodynamic design, modeling and stability. Mathematical model of the vehicle is obtained using the Euler-Lagrange formulation and includes aerodynamic parameters of the design. For the stability, a classic control law is proposed taking in account the aerodynamic parameters and the sensors bandwidth implemented in the aircraft. Simulation results are shown for the closed-loop system of the vehicle. Finally, aerodynamic design and avionics are based on flying and handling qualities for having a mini airplane that performs a reliable and stable flight.","PeriodicalId":6661,"journal":{"name":"2014 11th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)","volume":"42 9","pages":"1-6"},"PeriodicalIF":0.0000,"publicationDate":"2014-12-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2014 11th International Conference on Electrical Engineering, Computing Science and Automatic Control (CCE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICEEE.2014.6978297","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
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Abstract
This paper presents the development of a mini airplane UAV, focusing on the aerodynamic design, modeling and stability. Mathematical model of the vehicle is obtained using the Euler-Lagrange formulation and includes aerodynamic parameters of the design. For the stability, a classic control law is proposed taking in account the aerodynamic parameters and the sensors bandwidth implemented in the aircraft. Simulation results are shown for the closed-loop system of the vehicle. Finally, aerodynamic design and avionics are based on flying and handling qualities for having a mini airplane that performs a reliable and stable flight.
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