{"title":"不确定条件下飞行器组合的控制","authors":"Mohamad T. Shahab, Kévin Garanger, E. Feron","doi":"10.23919/ACC53348.2022.9867535","DOIUrl":null,"url":null,"abstract":"In this paper, we consider the problem of controlling a rigid assembly of aerial vehicles under uncertainty. We consider the case when the positions of the vehicle modules in the assembly structure are unknown, but belong to a finite set. In addition, we consider that each module has only its own measurements available for feedback but not that of the whole assembly, so a decentralized control law is developed. We apply an adaptive switching control approach to control this uncertain system. Given a stabilizing controller for the case when there is no uncertainty, we show that the proposed adaptive approach achieves the control objective under uncertainty by presenting illustrative simulation examples; we provide a case study of a recently proposed novel modular flying system, namely a fractal tetrahedron assembly.","PeriodicalId":366299,"journal":{"name":"2022 American Control Conference (ACC)","volume":"38 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2022-06-08","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Control of an Assembly of Aerial Vehicles Under Uncertainty\",\"authors\":\"Mohamad T. Shahab, Kévin Garanger, E. Feron\",\"doi\":\"10.23919/ACC53348.2022.9867535\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"In this paper, we consider the problem of controlling a rigid assembly of aerial vehicles under uncertainty. We consider the case when the positions of the vehicle modules in the assembly structure are unknown, but belong to a finite set. In addition, we consider that each module has only its own measurements available for feedback but not that of the whole assembly, so a decentralized control law is developed. We apply an adaptive switching control approach to control this uncertain system. Given a stabilizing controller for the case when there is no uncertainty, we show that the proposed adaptive approach achieves the control objective under uncertainty by presenting illustrative simulation examples; we provide a case study of a recently proposed novel modular flying system, namely a fractal tetrahedron assembly.\",\"PeriodicalId\":366299,\"journal\":{\"name\":\"2022 American Control Conference (ACC)\",\"volume\":\"38 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2022-06-08\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2022 American Control Conference (ACC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/ACC53348.2022.9867535\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2022 American Control Conference (ACC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/ACC53348.2022.9867535","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Control of an Assembly of Aerial Vehicles Under Uncertainty
In this paper, we consider the problem of controlling a rigid assembly of aerial vehicles under uncertainty. We consider the case when the positions of the vehicle modules in the assembly structure are unknown, but belong to a finite set. In addition, we consider that each module has only its own measurements available for feedback but not that of the whole assembly, so a decentralized control law is developed. We apply an adaptive switching control approach to control this uncertain system. Given a stabilizing controller for the case when there is no uncertainty, we show that the proposed adaptive approach achieves the control objective under uncertainty by presenting illustrative simulation examples; we provide a case study of a recently proposed novel modular flying system, namely a fractal tetrahedron assembly.