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卫星姿态控制系统硬件在回路仿真研究

Research on Hardware in the Loop Simulation for Satellite Attitude Control System

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【作者】 王宁强刘向东

【Author】 WANG Ning-qiang,LIU Xiang-dong(Beijing Institute of technology,Beijing 100081,China)

【机构】 北京理工大学自动控制系北京理工大学自动控制系 北京100081北京100081

【摘要】 为了便于卫星自主智能控制技术的研究,该文研究了控制系统硬件在回路仿真技术,分析了实时仿真系统中仿真步长的确定及通讯接口技术的应用。文中详细说明了在MATLAB下采用S-function编写串口驱动模块的方法,还介绍了利用MATLAB/xPC环境下的UDP模块进行数据传输的方法。最后,该文设计了一个基于PC机的三轴稳定卫星姿态控制硬件在回路仿真系统,将反作用飞轮、陀螺等实物接入仿真系统。仿真结果表明实时仿真结果与数学仿真结果基本一致,仿真系统接口设计合理,实时性符合要求。

【Abstract】 This paper discusses the hardware in the loop simulation of control system for the researches on the technology of satellite self-determination intelligent control,and analyzes the choosing of simulation step in real-time simulation and the application of the technology to communication interface.The method of building driver module for serial port with S-function based on MATLAB and the way of data transmission with the application of UDP module under MATLAB/xPC target environment are introduced and analyzed in details.At last,the hardware in the loop simulation system for three-axis stabilized satellite attitude control based on PC,with reaction wheel and gyro in the loop is designed.The results show the consistency of digital simulation and real-time simulation,the rationality of communication interface and the satisfaction of real-time characteristic.

  • 【文献出处】 计算机仿真 ,Computer Simulation , 编辑部邮箱 ,2005年10期
  • 【分类号】TP391.9
  • 【被引频次】15
  • 【下载频次】476
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