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Study on the control system of a hardware-in-loop micro-satellite simulator

机译:硬件在环微卫星模拟器的控制系统研究

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This paper presents a detailed control system building process for a hardware-in-loop micro-satellite simulator to apply and test system identification or control algorithms. It also designs a new system mechanism to combine the simulator with MATLAB Simulink by DDE, which can enable Simulink to directly control the simulator system and accomplish data sharing and real-time control function. Finally, it designs a controller based on the new control system structure to perform satellite attitude manoeuvre as system verification and gives out the result analysis for the future improvement. The control system building process may be a reference for other simulation environment's control system design.
机译:本文提出了一种用于硬件在环微卫星模拟器的详细控制系统构建过程,以应用和测试系统识别或控制算法。它还设计了一种新的系统机制,将模拟器与DDE的MATLAB Simulink相结合,可以使Simulink直接控制模拟器系统,并完成数据共享和实时控制功能。最后,设计了一种基于新控制系统结构的控制器,以进行卫星姿态操纵作为系统验证,并给出结果分析,以供将来改进。控制系统构建过程可能是其他仿真环境的控制系统设计的参考。

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