首页 | 本学科首页   官方微博 | 高级检索  
     

星载辐射计扫描镜太阳辐射热-结构建模与仿真
引用本文:游思梁,陈桂林,王淦泉. 星载辐射计扫描镜太阳辐射热-结构建模与仿真[J]. 中国空间科学技术, 2011, 31(1): 62-69. DOI: 10.3780/j.issn.1000-758X.2011.01.009
作者姓名:游思梁  陈桂林  王淦泉
作者单位:(1 上海交通大学航空航天学院,上海 200240)(2 中国科学院上海技术物理研究所,上海 200083)
摘    要:三轴稳定卫星平台搭载的光学有效载荷都存在午夜太阳辐射干扰问题,由此产生的热变形效应对光学系统的成像品质影响显著。采用复杂外热流近似建模技术,以及多软件耦合有限元仿真方法,以FY-4卫星的扫描辐射计为应用背景,研究了昼夜太阳辐射对星载辐射计扫描镜产生的热效应,并对不同热设计条件下的工况进行了对比分析。分析结果显示:扫描镜侧面及背面的热控涂层选取对其热变形有重要影响,但是仅仅通过热设计解决温度波动和热变形的矛盾是不够的,需要通过改进扫描镜的材料和优化光机结构加以改善。

关 键 词:扫描镜  太阳辐射  热效应  三轴稳定平台  卫星  
收稿时间:2010-03-26

Thermal-structural Modeling and Simulation for Scan Mirror on Imager in Solar Radiation
You Siliang,Chen Guilin,Wang Ganquan. Thermal-structural Modeling and Simulation for Scan Mirror on Imager in Solar Radiation[J]. Chinese Space Science and Technology, 2011, 31(1): 62-69. DOI: 10.3780/j.issn.1000-758X.2011.01.009
Authors:You Siliang  Chen Guilin  Wang Ganquan
Affiliation:(1 School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai 200240)(2 Shanghai Institute of Technical Physics,Chinese Academy of Sciences, Shanghai 200083)
Abstract:The solar-radiation disturbance exists in the optical payloads onboard the three-axis stabilized satellite platform. It leads to thermal distortion, which obviously affects the imaging quality of optical system. The approximate modeling technique of complex external heat flux was applied, as well as the multi-software-coupled finite element simulation. The thermal effect of the imager′s scan mirror caused by solar radiation was researched, and compared under different thermal design conditions on the FY-4 imager. The optimal scheme of the thermal design of the scan mirror was obtained. The result shows that the thermal distortion is closely related to the thermal coating on the side and the back of the scan mirror. It is difficult to resolve the conflict between the temperature fluctuation and the thermal distortion if only using the thermal design method. It is necessary to improve the material of the scan mirror or adjust the optical-mechanical structure.
Keywords:Scan mirror  Solar radiation  Thermal effect  Three-axis stabilized platform  Satellite  
本文献已被 万方数据 等数据库收录!
点击此处可从《中国空间科学技术》浏览原始摘要信息
点击此处可从《中国空间科学技术》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号