首页 | 本学科首页   官方微博 | 高级检索  
     

充液挠性飞行器的变结构控制
引用本文:彭冬亮,徐世杰,荆武兴.充液挠性飞行器的变结构控制[J].哈尔滨建筑大学学报,2003(10).
作者姓名:彭冬亮  徐世杰  荆武兴
作者单位:浙江大学工业控制技术国家重点实验室,北京航空航天大学宇航学院,哈尔滨工业大学航天学院 浙江 杭州310027,北京100083,黑龙江 哈尔滨150001
基金项目:国家自然科学基金(19872002)
摘    要:给出了带有多个挠性附件的充液飞行器的动力学方程,针对此模型采用变结构控制方法设计了系统的控制器。控制任务包括操纵天线使之跟踪事先给定的运动规律,并保持星体在惯性空间稳定,同时有效地抑制附件的弹性振动。通过仿真算例验证了此控制律的有效性。

关 键 词:充液挠性飞行器  动力学模型  变结构控制

Variable structure control of flexible liquid-filled spacecraft
PENG Dong-liang,XU Shi-jie,JING Wu-xing. National Laboratory of Industrial Control Technology,Zhejiang University,Hangzhou ,China,. College of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing ,China,. School of Astronautics,Harbin Institute of Technology,Harbin ,China.Variable structure control of flexible liquid-filled spacecraft[J].Journal of Harbin University of Civil Engineering and Architecture,2003(10).
Authors:PENG Dong-liang  XU Shi-jie  JING Wu-xing National Laboratory of Industrial Control Technology  Zhejiang University  Hangzhou  China  College of Astronautics  Beijing University of Aeronautics and Astronautics  Beijing  China  School of Astronautics  Harbin Institute of Technology  Harbin  China
Affiliation:PENG Dong-liang1,XU Shi-jie2,JING Wu-xing31. National Laboratory of Industrial Control Technology,Zhejiang University,Hangzhou 310027,China,2. College of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083,China,3. School of Astronautics,Harbin Institute of Technology,Harbin 150001,China
Abstract:Dynamics equations are given for liquid-filled spacecraft with several flexible appendages, and a controller is designed using the variable structure control strategy. The control mission consists of maneuvering the large antennas to track the pre-selected motion laws, stabilizing the satellite in an inertial space and sup- pressing the elastic vibration of the appendages. A numerical example is given to prove the validity of the con- trol laws.
Keywords:flexible liquid-filled spacecraft  dynamics model  variable structure control
本文献已被 CNKI 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号