{"title":"电磁/磁通量钉钉协同作用下航天器自与软对接控制方法","authors":"Yuan‐wen Zhang, Le-ping Yang, Yanwei Zhu","doi":"10.23919/CCC50068.2020.9189625","DOIUrl":null,"url":null,"abstract":"Spacecraft docking controlled by inter-craft electromagnetic fields actuation not only hasn’t propellant consumption and plume contamination, but also provides high-precision control capability of continuous, reversible, synchronous and non-contacting. In addition, with electromagnetic/magnetic flux-pinning synergy, spacecraft docking has 6-DOF passive stability, stiffness and damping effect. This paper deals with the optimized electromagnetic moment design for magnetic flux-pinning and the handover control approach between the two actuation phases. Finally, several numerical simulations are utilized to verify the theoretical design.","PeriodicalId":255872,"journal":{"name":"2020 39th Chinese Control Conference (CCC)","volume":"39 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-07-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"2","resultStr":"{\"title\":\"Spacecraft self- and soft-docking control approach with electromagnetic/magnetic flux-pinning synergy\",\"authors\":\"Yuan‐wen Zhang, Le-ping Yang, Yanwei Zhu\",\"doi\":\"10.23919/CCC50068.2020.9189625\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Spacecraft docking controlled by inter-craft electromagnetic fields actuation not only hasn’t propellant consumption and plume contamination, but also provides high-precision control capability of continuous, reversible, synchronous and non-contacting. In addition, with electromagnetic/magnetic flux-pinning synergy, spacecraft docking has 6-DOF passive stability, stiffness and damping effect. This paper deals with the optimized electromagnetic moment design for magnetic flux-pinning and the handover control approach between the two actuation phases. Finally, several numerical simulations are utilized to verify the theoretical design.\",\"PeriodicalId\":255872,\"journal\":{\"name\":\"2020 39th Chinese Control Conference (CCC)\",\"volume\":\"39 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"2020-07-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"2\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"2020 39th Chinese Control Conference (CCC)\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.23919/CCC50068.2020.9189625\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"2020 39th Chinese Control Conference (CCC)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.23919/CCC50068.2020.9189625","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
Spacecraft self- and soft-docking control approach with electromagnetic/magnetic flux-pinning synergy
Spacecraft docking controlled by inter-craft electromagnetic fields actuation not only hasn’t propellant consumption and plume contamination, but also provides high-precision control capability of continuous, reversible, synchronous and non-contacting. In addition, with electromagnetic/magnetic flux-pinning synergy, spacecraft docking has 6-DOF passive stability, stiffness and damping effect. This paper deals with the optimized electromagnetic moment design for magnetic flux-pinning and the handover control approach between the two actuation phases. Finally, several numerical simulations are utilized to verify the theoretical design.
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