小卫星姿态轨道控制系统地面试验平台

2014 International Conference on Mechatronics and Control (ICMC) Pub Date : 2014-07-03 DOI:10.1109/ICMC.2014.7231780

Li Hua-yi

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引用次数: 1

摘要

设计了小卫星姿态轨道控制系统地面试验平台。仿真了实际传感器/执行器与车载计算机之间的硬件接口。对卫星动态环境和空间环境进行计算，形成闭环控制系统。最后，通过对比仿真结果和在轨飞行数据，对地面试验系统进行了验证。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Ground test platform for attitude and orbit control system of small satellite

Ground test platform for attitude and orbit control system of small satellite is designed. Hardware interfaces between the real sensors/actuators and the onboard computer is simulated. Satellite dynamic and space environment is calculated in order to form a close-loop control system. Finally, the ground test system is validated by comparing the simulation result and in-orbit flying data.

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2014 International Conference on Mechatronics and Control (ICMC)

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