卫星太阳电池阵动力学研究综述  

Review on Satellite Solar Array Dynamics

作　　者：田林 郭丽华 吴怡 陆文浩 李逸凡 翁子豪 TIAN Lin;GUO Lihua;WU Yi;LU Wenhao;WENG Zihao(School of Mechanical Engineering,Suzhou University of Science and Technology,Suzhou 215009)

机构地区：[1]苏州科技大学机械工程学院,苏州215009

出　　处：《现代制造技术与装备》2018年第10期123-123,125,共2页Modern Manufacturing Technology and Equipment

基　　金：江苏省高等学校大学生创新创业训练计划(项目编号:201610332019Z);苏州科技大学青年基金项目(项目编号:341511403)

摘　　要：太阳电池阵是卫星上至关重要的组成部分,它为卫星的在轨工作提供电力,太阳电池阵的顺利展开对卫星能正常工作有决定性的影响。太阳阵的展开和锁定过程会发生复杂的刚柔耦合动力学行为,太阳阵的展开会对卫星本体造成冲击,引起卫星本体的姿态发生变化。本文对卫星太阳电池阵动力学与控制问题研究的发展和现状进行了综述并对其发展趋势做了探讨。The solar array is a vital component of the satellite. It provides power for the satellite’s on-orbit operation. The successful unfolding of the solar array has a decisive impact on the satellite’s normal operation. During the unfolding and locking process of the solar array, complex rigid-flexible coupled dynamic behavior occurs, and the unfolding of the solar array will impact the satellite body , causing the attitude of the satellite body to change. In this paper, the development and current status of research on the dynamics and control of satellite solar arrays were reviewed and their development trends were discussed.

关 键 词：太阳电池阵 动力学 碰撞 姿态控制 

分 类 号：V442[航空宇航科学与技术—飞行器设计]