包络球与空间气球间温度分布及红外辐射特性的差异
[1] Tidrow M Z, Dyer W R. Infrared sensors for ballistic missile defense[J]. Infrared Physics & Technology, 2001, 42(3/5): 333-336.
[2] 黄伟,吉洪湖.蒙皮反射的背景辐射对亚音速飞机红外特征的影响研究(一):方法[J].红外与激光工程,2015,44(6):1699-1703.
[3] 石良臣,朱定强,蔡国飙.卫星多光谱信号的仿真研究[J].光电工程,2009,36(5):40-46.
[4] 郭明,王学伟.空间目标/星空背景红外建模与仿真[J].红外与激光工程,2010,39(3):399-404.
GUO Ming, WANG Xuewei. IR modeling and simulation of space target/star and space environment[J]. Infrared and Laser Engineering, 2010, 39(3): 399-404.
[5] Dan D V Bhanderi, Thomas Bak. Modeling earth albedo for satellite in earth orbit[C]//AIAA, 2005: DOI:.10.2514/6.2005-6465.
[6] ZHANG Jun. Finite element analysis of the surface temperature distribution on the exoatmospheric ballistic target[J]. Infrared and Laser Engineering, 2008, 37(3): 416-419.
[7] WU X D, HUANG C C, LING Y, et al. Surface temperature and infrared feature of a satellite[J]. Infrared and Laser Engineering, 2011, 40(5): 805-810.
杨星, 吴晓迪, 陈杰. 包络球与空间气球间温度分布及红外辐射特性的差异[J]. 红外技术, 2018, 40(4): 395. YANG Xing, WU Xiaodi, CHEN Jie. Differences of Temperature Distribution and Infrared Radiation Feature Between Envelope Balloon and Spatial Balloon[J]. Infrared Technology, 2018, 40(4): 395.