杨黔龙, 周凤岐. 基于Windows的滑翔增程弹飞控系统半实物仿真研究[J]. 微电子学与计算机, 2012, 29(4): 154-157.
引用本文: 杨黔龙, 周凤岐. 基于Windows的滑翔增程弹飞控系统半实物仿真研究[J]. 微电子学与计算机, 2012, 29(4): 154-157.
YANG Qian-long, ZHOU Feng-qi. Semi-physical Simulation of the Gliding Missile Flight Control System Based on Windows Operation System[J]. Microelectronics & Computer, 2012, 29(4): 154-157.
Citation: YANG Qian-long, ZHOU Feng-qi. Semi-physical Simulation of the Gliding Missile Flight Control System Based on Windows Operation System[J]. Microelectronics & Computer, 2012, 29(4): 154-157.

基于Windows的滑翔增程弹飞控系统半实物仿真研究

Semi-physical Simulation of the Gliding Missile Flight Control System Based on Windows Operation System

  • 摘要: 通过引入外部硬时钟,在普通Windows工控机上,实现了精确定时以及稳定的多线程串口通信,满足了滑翔弹飞控系统实时仿真的要求.该系统不仅成本低,而且稳定性高、通用性好以及第三方软硬件资源丰富,并在实际仿真过程中得到了应用.

     

    Abstract: A semi-physical simulation platform in use of windows operation system is successfully established bases on general industrial PC combined with an external timer,the precise timing and steady multithreading serial communication are realized.The system is proved satisfying the real-time simulation requirement of the gliding missile.The novel platform could not only low-cost,but also is precise and universal,which has been successfully used in the semi-physical simulation practice of a gliding missile.

     

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