太空应用太阳位置传感器的设计和模拟:一项比较研究
Martha Díaz Salazar1,2, Nadia Kondratiuk1,2, Analía Moreno1,2
1Departamento Energía Solar - Comisión Nacional de Energía Atómica (CNEA), General Paz 1499 CP1650, San Martín, Buenos Aires, Argentina.
The Review of scientific instruments
|July 10, 2024
概括
这项研究详细介绍了太阳位置传感器的设计,用于航天器的态度控制. 通过分析窗口和探测器配置来优化传感器设计,以提高灵敏度和线性.
科学领域:
- 太空飞船工程 太空飞船工程
- 光学传感器设计的设计
- 摄影检测技术的技术.
背景情况:
- 太阳位置传感器是航天器姿态确定和控制系统中的关键组件.
- 精确的太阳跟踪对于太空应用中的电力管理和任务成功至关重要.
研究的目的:
- 描述单轴和双轴太阳位置传感器的设计过程.
- 为了建模,模拟和比较各种基于光二极管阵列和光学窗口的传感器架构.
主要方法:
- 开发并模拟了六种不同的传感器架构,具有不同的探测器和窗口几何形状.
- 通过分析窗口高度/尺寸和光电极尺寸的影响来评估传感器性能.
- 比较探测器配置 (例如,二象限与三角形) 和窗口形状 (例如,方形).
主要成果:
- 关键性能因素包括窗口高度,窗口/光电模尺寸,探测器配置和窗口几何形状.
- 与三角光二极管相比,两象限探测器配置显示出更高的灵敏度.
- 发现一个方形窗口设计可以增强输出线性.
结论:
- 检测器配置和窗口几何的选择显著影响太阳传感器的灵敏度和线性.
- 优化窗口和探测器参数对于在太空应用中实现所需性能至关重要.
- 这项研究支持开发新的太空产品和阿根廷国家太空计划.
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