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万有引力场中带挠性附件充液卫星的姿态稳定性
引用本文:成功,刘延柱.万有引力场中带挠性附件充液卫星的姿态稳定性[J].空间科学学报,1997,17(4):367-371.
作者姓名:成功  刘延柱
作者单位:上海交通大学工程力学系
基金项目:国家自然科学基金,博士点专项科研基金
摘    要:本文利用能量-Casimir方法讨论万有引力场中带挠性附件非对称全充液卫星的姿态稳定性, 导出此刚-弹-液系统在轨道坐标系内相对平衡的稳定性充分条件. 

关 键 词:姿态稳定性    能量    Casimir方法    充液系统动力学
收稿时间:1996-11-12

ATTITUDE STABILITY OF LIQUID-FILLED SATELLITE WITH FLEXIBLE APPENDAGE IN GRAVITATIONAL FIELD
CHENG Gong, LIU Yanzhu.ATTITUDE STABILITY OF LIQUID-FILLED SATELLITE WITH FLEXIBLE APPENDAGE IN GRAVITATIONAL FIELD[J].Chinese Journal of Space Science,1997,17(4):367-371.
Authors:CHENG Gong  LIU Yanzhu
Institution:Dept of Engineering Mechanics Shanghai Jiao Tong Uhiversity, 200030
Abstract:The atutude stability of an asymmetrical liqind-filled satellite with a flexible barin the gravitational field by using the Energy-Casimir method is discussed in presentPaper. A sufficient condihon of stability of the relative equllibritim of the rigidelashc- liquld system in the orbtal coordinates is obtained. It is shown that thestablity condihon for such a system has a formal idenhty with the condihon of arigid satellite in the gravitahoal field.
Keywords:Attitude stability  Energy-Casimir method  Dynamics of liquid-filled system
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