采用线性CMOS探测器的两轴微型数字式太阳敏感器的设计与研制

A. Maji, H. R. Prabhamani, Veena John, H. S. Ravindra, K. Subhalakshmi, A. S. Laxmiprasad
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引用次数: 3

摘要

本文介绍了用于印度卫星任务的高精度、紧凑、双轴微型数字太阳敏感器(Micro DSS)的设计细节,该传感器采用线性互补金属氧化物半导体探测器和n形狭缝掩膜。由于质量小,体积小,功耗低,微型数字太阳传感器非常适合未来的微/纳米卫星以及通信卫星形成太阳传感器网络。在光电系统实验室建立了微型数字太阳敏感器的电学模型。它比印度空间研究组织(ISRO)目前可用的高精度太阳传感器轻8倍,紧凑25倍。Micro DSS在太阳传感器校准设备前进行测试,精度达到0.02°。在本文中,我们还详细介绍了Micro DSS的测试结果。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and development of two axes micro digital sun sensor using linear CMOS detector
This paper presents the design details of newly developed high accuracy, compact, two axes Micro Digital Sun Sensor (Micro DSS) using linear Complementary Metal Oxide Semiconductor detector and N-shaped slit mask for Indian Satellite missions. Due to low mass, compact size and low power, the Micro Digital Sun Sensor is very much suitable for future micro/ nano-satellites as well as for communication satellites to form a Sun sensors network. The electrical model of Micro Digital Sun Sensor is built in Laboratory for Electro-Optics Systems (LEOS). It is eight times lighter and twenty five times more compact than the presently available high accuracy Sun sensor in Indian Space Research Organization (ISRO). The Micro DSS is tested in front of the Sun sensor calibration facility and accuracy of 0.02° is achieved. In this paper, we have also presented details of the test results of Micro DSS.
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