Based on the working principle of the small P13XM015-TFT-LCD star simulator and its designing, manufacturing, processing, debugging and detection technology of the whole system during the engineering application, the detection method for the two parameters of the small star simulator such as intersatellite spacing and magnitude was studied. The inter-satellite spacing was corrected by software then measured respectively and recombined to be corrected, while the adapted instrument magnitude method was used for the magnitude testing. The optical system collimating lens, preparation of simulator star database, coordinate transformation, position calculating, and system control software of the small star simulation system were designed by using modularity method. The assembly of the entire system was implemented in the laboratory, the controlling and testing platform was set up, and then the experimental results were obtained. The results show that, this system has high reliability with star database precision and position calculating error of no more than 2and angular resolution error of no more than 3.43.
ZHANG Jie, ZHANG Tao, KUANG She-qing.
Design of small star simulator system. Journal of Applied Optics. 2013, 34(6): 920-927
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参考文献
[1]樊靖中-空间光学姿态敏感器的发展[J]控制工程,1986(6):13-16 FAN Jing-zhong-The development of space optical attitude sensors[J]- Control Engineering,1986(6):13-16(in Chinese with an English abstract) [2]朱耆祥-白天用.CCD 摄像机对天体目标的探测及实验[J].光电工程,1995,22(6):1-10 ZHU Ji-xiang,BAI Tian-yong.CCD camera for celestial object detection and experiment[J]-The Photoelectric Engineering 1995,22(6):13-16- (in Chinese with an English abstract) [3]SMITH J L ,WHITFORD C-小卫星的低成本姿态确定与控制[J]控制工程,1998(2):41-53 SMITH J L,WHITFORD C-The low cost of small satellite attitude determination and control[J]- Control Engineering ,1998(2):41-53-(in Chinese with an English abstract) [4]SGHEDONI M-多任务航天器平台的姿态和轨道控制系统[J]控制工程,1997(5):32-40 SGHEDONI M-Multimission platform for spacecraft attitude and orbit control systems[J].Control Enginee