{"title":"Multi-vehicle circular formation flight in an unknown time-varying flow-field","authors":"Mohammad H. Sadraey","doi":"10.1109/ICUAS.2013.6564770","DOIUrl":null,"url":null,"abstract":"This paper presents a coordination technique for circular formation flight of multiple Unmanned Aerial Vehicles (UAVs) to circle around a ground target when a wind with an unknown velocity and direction is blowing. The guidance law is based on the line-of-sight (LOS) method which has the ability to transfer UAVs to different formation patterns through a single parameter change. An optimal control law is applied to a linear dynamic model employing a linear quadratic regulator (LQR) control technique. A leader-follower coordination model is adopted for encirclement around the ground target. In order to verify the performance of the proposed system, a numerical simulation is demonstrated.","PeriodicalId":322089,"journal":{"name":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","volume":"1 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2013-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2013 International Conference on Unmanned Aircraft Systems (ICUAS)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/ICUAS.2013.6564770","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 5
Abstract
This paper presents a coordination technique for circular formation flight of multiple Unmanned Aerial Vehicles (UAVs) to circle around a ground target when a wind with an unknown velocity and direction is blowing. The guidance law is based on the line-of-sight (LOS) method which has the ability to transfer UAVs to different formation patterns through a single parameter change. An optimal control law is applied to a linear dynamic model employing a linear quadratic regulator (LQR) control technique. A leader-follower coordination model is adopted for encirclement around the ground target. In order to verify the performance of the proposed system, a numerical simulation is demonstrated.