欢迎您！东篱公司
退出
-
申报数据库
-
立项数据库
-
成果数据库
-
项目获奖数据库
中文摘要：
在ADAMS软件平台上建立了航天器太阳帆板展开过程动力学虚拟样钡模型，研究了目前航天器太阳帆板典型的三种布局安装方式，分别为太阳帆板安装在航天器一侧同步展开；太阳帆板安装在航天器两侧同步展开；太阳帆板安装在四侧同步展开。对三种布局安装方式下的太阳帜板展开过程进行了动力学仿真并对仿：茸结果进行了比较，仿真结果可以准确的预测三种布局安装方式下太阳帆板展开过程的动力学特性以及帜掘展开过程时航天器誉体姿态运动的影响，可以为航天器太阳帆板布局方案提供参考，有利于初期方案的筛选，也为航天器姿态控制系统的设计以及地面试验系绫提供参考依据。
英文摘要：
The dynamics virtual prototype model of deployment of solar panels was built on ADAMS. Three typical layouts for solar panel of spacecraft were analyzed： the first layout is the panels on one side of spacecraft deployed synchronously; the second layout is the panels on two sides of spacecraft deployed synchronously; the third layout is the panels on four sides of spacecraft deployed synchronously. The dynamics simulation of deployment of solar panels was made and the results were compared. The simulation results can predict the deployment dynamics characters of solar panels and the effects of deployment of solar panels on satellite attitude motion preferably in three typical layouts. It has some reference meaning to the layout of solar panels on spacecraft and it is propitious to select scheme at beginning. And it can be reference for engineering design of spacecraft control system and ground text.
同期刊论文项目
同项目期刊论文
期刊信息
位置：