摘要
以概率论的基本原理为依据，分析和计算了阳光直射对空间光学遥感器的外遮光罩的辐射加热，其中包括不同轨道位置处飞船船体对阳光的遮挡和阳光从外遮光罩开口处斜入射到其内腔的情况。
According to the probability theory,the solar radiation to the outer baffle of optical remote sensor has been analyzed and calculated,including the different shadow conditions of the spacecraft and the solar oblique radiation from the opening of the outer baffle to the inner cavity.The projective geometry calculation of the complex surfaces of second order is avoided.
出处
《光学精密工程》
EI
CAS
CSCD
1997年第1期28-34,共7页
Optics and Precision Engineering
基金
国家自然科学基金
关键词
外遮光罩
宇宙飞船
辐射换热
空向遥感器
Random simulation,Solar radiation,Outer baffle,Spacecraft,Radiation heat transfer
