{"title":"具有参数不确定性的多架垂直起降飞机鲁棒编队控制","authors":"Yu-Chan Chen, B. Ma","doi":"10.1109/CGNCC.2016.7828792","DOIUrl":null,"url":null,"abstract":"In this work, the formation control problem is investigated for a group of planar vertical take-off and landing (PVTOL) aircraft. By combining the input-output linearization technology and the nonlinear time-varying tool, a distributed sliding-mode formation controller is derived guaranteeing that the multiple PVTOL aircraft come into a desired stationary formation shape with the velocities and the roll angle convergent to zero. The formation errors are showed to be asymptotically convergent to zero. Simulation results show the effectiveness of the proposed formation control algorithm.","PeriodicalId":426650,"journal":{"name":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","volume":"73 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2016-08-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Robust formation control of multiple PVTOL aircraft with parameter uncertainties\",\"authors\":\"Yu-Chan Chen, B. Ma\",\"doi\":\"10.1109/CGNCC.2016.7828792\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this work, the formation control problem is investigated for a group of planar vertical take-off and landing (PVTOL) aircraft. By combining the input-output linearization technology and the nonlinear time-varying tool, a distributed sliding-mode formation controller is derived guaranteeing that the multiple PVTOL aircraft come into a desired stationary formation shape with the velocities and the roll angle convergent to zero. The formation errors are showed to be asymptotically convergent to zero. Simulation results show the effectiveness of the proposed formation control algorithm.\",\"PeriodicalId\":426650,\"journal\":{\"name\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"volume\":\"73 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2016-08-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1109/CGNCC.2016.7828792\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2016 IEEE Chinese Guidance, Navigation and Control Conference (CGNCC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CGNCC.2016.7828792","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Robust formation control of multiple PVTOL aircraft with parameter uncertainties
In this work, the formation control problem is investigated for a group of planar vertical take-off and landing (PVTOL) aircraft. By combining the input-output linearization technology and the nonlinear time-varying tool, a distributed sliding-mode formation controller is derived guaranteeing that the multiple PVTOL aircraft come into a desired stationary formation shape with the velocities and the roll angle convergent to zero. The formation errors are showed to be asymptotically convergent to zero. Simulation results show the effectiveness of the proposed formation control algorithm.
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