Dynamics Simulation of Deployment of Solar Panels on Oblique Spacecraft

摘要：

The dynamics simulation of deployment of a solar panel on an oblique spacecraft is presented.For the case of the solar panel installed on the oblique spacecraft,the dynamics model of the spacecraft is established using the software ADAMS.Based on the dynamics model,the dynamics simulations of deployment for the solar panel on the special oblique spacecraft are presented.The simulation results are compared with a common spacecraft on which the solar panel is installed normally.The comparison of the results indicates that the special oblique spacecraft causes obvious changes in the attitude motion of the spacecraft and the yaw angle of spacecraft changes greatly only in the special oblique spacecraft system.However the changes in roll and pitch are slight.The difference of the attitude motion between two kinds of spacecrafts is significant.The simulation results can predict the attitude motion of the oblique spacecraft and deployment dynamics of solar panel preferably and it is useful for control system design and ground text of the special oblique spacecrafts.

作者: Zhengfeng Bai Yang Zhao Hao Tian

会议类型: 国际会议

会议名称: Asia Simulation Conference 2008/the 7th International Conference on System Simulation and Scientific Computing(2008亚洲仿真会议/第七届系统仿真和科学计算国际会议)(ICSC2008)

会议地点: 北京

会议语种:英文

在线出版日期: 2008-10-10（万方平台首次上网日期，不代表论文的发表时间）