空间导航系统姿态控制用太阳跟踪器

Antonio de la Calle-Martos, Rubén Gómez-Merchán, J. A. Leñero-Bardallo, Á. Rodríguez-Vázquez
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引用次数: 0

摘要

我们报告一种用于空间导航系统姿态控制的太阳跟踪传感器。该传感器利用了作者先前为这些设备设计的异步操作概念。异步亮度传感器优化太阳跟踪器的操作,因为只有被照亮的像素被读出并可以传输数据。这种方法在带宽消耗、延迟和功耗方面优于传统的基于帧的太阳跟踪器。正在研究的新型传感器已经优化了操作和与其他姿态控制系统的交互。传感器的功耗大大降低。为了节省电力,它的像素在测量照明水平后自动进入待机模式。该器件的工作电压仅为0.45V。像素矩阵被设计为可选地直接由基于连接到存储电容的光伏二极管的能量收集系统供电,而不需要DC-DC转换器。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Sun tracker sensor for attitude control of space navigation systems
We report a sun tracker sensor for attitude control of space navigation systems. The sensor exploits the concept of asynchronous operation previously devised by the authors for those devices. Asynchronous luminance sensors optimize sun trackers operation because only illuminated pixels are readout and can transmit data. This approach outperforms classic frame-based sun trackers in terms of bandwidth consumption, latency, and power consumption. The new sensor under study has been optimized for operation and interaction with other attitude control systems when it is embarked. The sensor power consumption is quite reduced. To save power, its pixels enter automatically in standby mode after gauging illumination levels. The device operates with only 0.45V. The pixel matrix has been devised to optionally be directly powered by energy harvesting systems based on photovoltaic diodes connected to a storage capacitor without a DC-DC converter.
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