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dc.contributor.author兰彭洪
dc.contributor.author罗林开
dc.contributor.author陈亚陵
dc.date.accessioned2017-11-14T01:29:03Z
dc.date.available2017-11-14T01:29:03Z
dc.date.issued2001-12-30
dc.identifier.citation厦门大学学报(自然科学版),2001,(S1):18-24
dc.identifier.issn0438-0479
dc.identifier.otherXDZK2001S1004
dc.identifier.urihttps://dspace.xmu.edu.cn/handle/2288/142266
dc.description.abstract研究多挠性充液卫星姿态运动的低阶鲁棒控制器设计问题.综合应用模态截断、H∞回路成形和H∞氏平衡截断方法设计低阶鲁棒控制器.模态截断获得适当阶数的卫星姿态运动模型;H∞回路成形方法设计鲁棒控制器;H∞平衡截断技术实现控制器降阶.满阶对象和低阶控制器组成闭环进行计算机仿真.
dc.description.abstractThis paper studies the reduced-order robust controller design of flexible satellite attitude. Mode truncation, H∞loop-shaping and H∞balanced truncation are being used during the controller designing. The model of satellite attitude movement is simplified by mode truncation, an robust controller is designed by H∞loop-shaping, and then, the robust controller is reduced by H∞balanced truncation. The closed-loop system, consisted by the reduced-order robust controller and the full-order plant, is simulated by computer.
dc.description.sponsorship中国空间技术研究院预研课题;; 教育部重点211工程项目
dc.language.isozh_CN
dc.subject姿态控制
dc.subject控制器降阶
dc.subject模态截断
dc.subjectH∞平衡截断
dc.subjectmode truncation
dc.subjectattitude conirol
dc.subjectcontroller reduction
dc.subjectH∞ balanced truncation
dc.title挠性卫星姿态低阶鲁棒控制器设计
dc.title.alternativeReduced-order Robust Controller Design of Flexible Satellite Attitude
dc.typeArticle


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