Shuailei Wang, Shaolei Zhou, Xuanbing Liu, Feiyang Dai, Yahui Qi, S. Yan
{"title":"Distributed Event-triggered Group Attitude Coordinated Control of Multi-spacecraft with Undirected Topology","authors":"Shuailei Wang, Shaolei Zhou, Xuanbing Liu, Feiyang Dai, Yahui Qi, S. Yan","doi":"10.1109/CACRE50138.2020.9229904","DOIUrl":null,"url":null,"abstract":"Group attitude coordinated control of multi-spacecraft is investigated with the distributed event-triggered mechanism. The communication topology of the system is an undirected graph. An auxiliary variable is designed, and event-triggered functions for every spacecraft are constructed. The control input is proposed with the information of the neighbor at the triggering instant. It is proved that the multi-spacecraft system can reach group attitude coordination, and for every spacecraft, the triggering interval has a positive lower bound, thus Zeno behavior is avoided. The effectiveness of the control input proposed is verified with simulation results.","PeriodicalId":325195,"journal":{"name":"2020 5th International Conference on Automation, Control and Robotics Engineering (CACRE)","volume":"148 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 5th International Conference on Automation, Control and Robotics Engineering (CACRE)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/CACRE50138.2020.9229904","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
Group attitude coordinated control of multi-spacecraft is investigated with the distributed event-triggered mechanism. The communication topology of the system is an undirected graph. An auxiliary variable is designed, and event-triggered functions for every spacecraft are constructed. The control input is proposed with the information of the neighbor at the triggering instant. It is proved that the multi-spacecraft system can reach group attitude coordination, and for every spacecraft, the triggering interval has a positive lower bound, thus Zeno behavior is avoided. The effectiveness of the control input proposed is verified with simulation results.