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基于dSPACE的微型核仿真验证系统
引用本文:王继河,王峰,施梨,常建松,曹喜滨. 基于dSPACE的微型核仿真验证系统[J]. 系统工程与电子技术, 2007, 29(12): 2149-2153
作者姓名:王继河  王峰  施梨  常建松  曹喜滨
作者单位:哈尔滨工业大学卫星技术研究所,黑龙江,哈尔滨,150080
基金项目:国家重点基础研究发展计划(973计划)
摘    要:为验证微型核原理样机软/硬件实时性能,采用dSPACE实时仿真器建立以微型核为核心的实时仿真验证系统。针对搭建微型核实时仿真验证系统的要求,重点解决了如何用dSPACE仿真器模拟外部实时仿真环境,以及微型核CAN总线和dSPACE仿真器RS232串口之间数据转换的难题。在系统成功建立的基础上,进行了小卫星姿态控制全模式实时仿真,完成了对微型核实时软/硬件性能的测试。仿真结果证明了本仿真验证系统软/硬件结构的正确性。

关 键 词:卫星  微型核  串口模型
文章编号:1001-506X(2007)12-2149-05
修稿时间:2006-11-07

dSPACE-based micro core simulation system
WANG Ji-he,WANG Feng,SHI Li,CHANG Jian-song,CAO Xi-bin. dSPACE-based micro core simulation system[J]. System Engineering and Electronics, 2007, 29(12): 2149-2153
Authors:WANG Ji-he  WANG Feng  SHI Li  CHANG Jian-song  CAO Xi-bin
Abstract:To verify the performance of the software and hardware of micro core,a real-time simulation system based on micro core is established by using dSPACE simulation system.According to the requirements of building the real-time simulation system,some technical problems are solved,such as how to use dSPACE system to simulate exterior real-time simulation environments and the data transformation between CAN bus of micro core and serial RS232 of dSPACE.Then,after successfully building the real-time simulation system,the full-mode attitude control simulation is performed to test the real-time performance of software and hardware of micro core.The result of the simulation demonstrates the validity of the software and hardware architecture of this real-time simulation system.
Keywords:dSPACE
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