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卫星天线双轴定位系统虚拟样机动力学仿真

李长江,廖瑛,廖超伟,冯向军   

  1. 中国空间技术研究院,国防科学技术大学航天与材料工程学院,国防科学技术大学航天与材料工程学院,国防科学技术大学航天与材料工程学院 北京100086 ,长沙410073 ,长沙410073 ,长沙410073
  • 发布日期:2005-10-25

The Dynamic Simulation of the Virtual Prototype of the Two-axes Position Mechanism for Satellite Antennas

Li Changjiang(China Academy of Space Technology,Beijing 100086)Liao Ying Liao Chaowei Feng Xiangjun(Institute of Aerospace and Material Engineering,National University of Defense Technology,Changsha 410073)   

  • Online:2005-10-25

摘要: 首先概述了双轴定位系统工作原理,在对系统结构进行分析、简化的基础上建立了双轴定位系统三维实体模型。其次,详细说明了基于三维实体模型的虚拟样机建模方法。然后,对虚拟样机进行了运动学和动力学仿真,并针对仿真结果进行深入细致分析,为卫星天线双轴定位系统物理样机的优化设计提供了技术支持。

关键词: 卫星天线, 定位系统, 动力学仿真

Abstract: Firstly,the work principle of the two-axes position mechanism for(satellite) antennas is indicated.A solid model of the two-axes position mechanism is built based on the(analysis) and simplification to the system.Then,the method of building the virtual prototype model based on the solid model is brought forth.Finally,the simulation results and the deep-going(analyzing)(conclusions) are showed,which provided the useful suggestions to the optimal design of the physical prototype of the two-axes position mechanism for satellite antennas.