摘要
Abstract
The ignition process of solid rocket motor is analyzed , then a solid rocket motor ignition control device is designed for the demand of ignition motor .This device with PLC as control core to exe-cute ignition action , with industrial PC as operation platform to complete parameter settings , its software platform uses LabVIEW graphical programming language of NI company .The application interface of this ignition device is simple intuitive , simple operation , safe and reliable , and it can better meet the multiple types of solid rocket engine test ignition test requirements .关键词
LabVIEW/固体火箭发动机/点火控制/可编程控制器Key words
LabVIEW/solid rocket motor/ignition control/PLC分类
航空航天
