Design of a Nanosatellite Attitude Control Hardware-in-the-loop Simulation System

Yong-Seok Lee, Nguyen Xuan Mung, Truong-Dong Do, Joon-Young Park, C. Lee, S. Hong
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Abstract

With the development of space technology, the missions of modern satellites are becoming more complicated. Therefore, it is essential to maintain a satellite’s attitude to perform specific missions successfully. Sending satellites into space is time-consuming and expensive, making their on-ground testing necessary and crucial. This paper proposes a hardware-in-the-loop simulation system to verify the satellite attitude control system. The hardware-in-the-loop simulation system is a low-cost solution for mimicking a gravity-free environment, allowing the satellite attitude control to perform as it will be in space.
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纳米卫星姿态控制半实物仿真系统设计
随着空间技术的发展,现代卫星的任务越来越复杂。因此,保持卫星的姿态对成功执行特定任务至关重要。将卫星送入太空既耗时又昂贵,因此地面测试是必要且至关重要的。本文提出了一种硬件在环仿真系统来验证卫星姿态控制系统。硬件在环仿真系统是一种低成本的解决方案,用于模拟无重力环境,允许卫星在太空中执行姿态控制。
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