面阵CCD电子线路在星敏感器设计中的应用  

The Application of Area Array CCD Electronics in Star-Sensor Design on Spacecraft

作　　者：杨威[1] 赵健翔[1] 

机构地区：[1]北京控制工程研究所

出　　处：《航天控制》1996年第3期24-29,共6页Aerospace Control

摘　　要：本文阐述了星敏感器的工作原理和系统要求，讨论了面阵ＣＣＤ在星敏感器中的应用方法，提出了星敏感器关键敏感器件的线路实现方案，对星敏感器硬件电路的设计进行了分析和研究，并在此基础上对实际电路进行了测试，分析了测试结果。This paper addresses the operating principle and system requirements of star-sensor on satellites. Based on area array charge-coupled device (CCD) as the key sensor, it elaborates a set of electronic design which is studied and analysed in detail here to meet the requirements for star-sensor system. Not only the real hardware has been implemented but also the test results and electronic features are presented.

关 键 词：航天器 星敏感器 姿态控制 CCD 

分 类 号：V448.22[航空宇航科学与技术—飞行器设计]