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为满足火箭增压系统试验平台的功能性及通用性等要求,设计了一套基于PLC的控制系统,硬件采用以太网和Profibus总线的网络架构方式,软件程序采用模块化和参数化的设计方法。经验证:该控制系统使得试验平台灵活地适用于各型号火箭增压系统的试验。
In order to meet the requirements of rocket booster system test platform such as functionality and versatility, a set of control system based on PLC is designed. The hardware adopts the network architecture of Ethernet and Profibus. The software program adopts the modular and parametric design method . Proven: The control system makes the test platform flexible for all types of rocket booster system test.