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dc.contributor.author兰维瑶
dc.contributor.author陈亚陵
dc.date.accessioned2016-05-17T02:46:06Z
dc.date.available2016-05-17T02:46:06Z
dc.date.issued1999
dc.identifier.citation厦门大学学报(自然科学版),1999,(2):41-46
dc.identifier.issn0438-0479
dc.identifier.otherXDZK902.006
dc.identifier.urihttps://dspace.xmu.edu.cn/handle/2288/106069
dc.description.abstract研究H∞/μ综合方法在新型卫星姿态运动的鲁棒控制器设计中的应用.讨论新型卫星姿态运动中卫星姿态控制以及挠性体振动抑制和液体晃动抑制等问题,同时阐述一个确定低阶控制器阶数的判据.
dc.description.abstractThe robust controller design of liquid satellite′s attitude movement was studied by using H ∞/μ method.Attitude control, as well as the suppression of the flexible structure′s vibration and the liquid sloshing, was discussed.A test for deciding the order of reduced order controller was formulated.
dc.description.sponsorship中国空间技术研究院预研资助
dc.language.isozh_CN
dc.subjectH_∞/μ综合
dc.subject挠性结构
dc.subject液体晃动
dc.subject控制器降阶
dc.subjectH ∞/μ Synthesis
dc.subjectFlexible structure
dc.subjectLiquid sloshing
dc.subjectController reduce
dc.title新型卫星姿态运动的鲁棒控制器设计
dc.title.alternativeRobust Controller Design of New Style Satellite′s Attitude Movement
dc.typeArticle


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