基于ABAQUS的空间机械臂锁紧点位置确定及受力分析
Locking positioning and reaction force analysis of the space arm based on ABAQUS
为确定最优的锁紧位置和锁紧点数目,在ABAQUS中建立了六自由度空间机械臂及其锁紧机构的有限元模型,首先初定几个关键的锁紧位置,然后以提高基频、降低相机响应为目标,分别分析锁紧位置、锁紧机构刚度、锁紧点数量对它们的影响,最终确定一组最优的锁紧点位置和锁紧点数目。依据发射过程中加速度量级,在所选取的锁紧位置下,计算锁紧点约束反力,依此可作为锁紧机构设计的输入。
o obtain the optimal locking position and locking point number, the finite element model was established in ABAQUS. In this paper we obtain some key lock points based on mode analysis first, and then put the high first mode frequency of the arm and low response of the camera as the aim. Through analyzing the effects of three factors: the locking location, locking mechanism stiffness and locking point number, at last , the most appropriate locking scheme is concluded. Based on the acceleration during launch, the reaction force in the locking position can be calculated, which can be used as the input for the design of the locking mechanism.
陈正升、刘明、孔民秀
航空航天技术机械设计、机械制图机械零件、传动装置
机械设计结构动力学模态分析BAQUS
Mechanical designStructural dynamicsModal AnalysisABAQUS
陈正升,刘明,孔民秀.基于ABAQUS的空间机械臂锁紧点位置确定及受力分析[EB/OL].(2013-03-07)[2025-08-05].http://www.paper.edu.cn/releasepaper/content/201303-270.点此复制
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