摘要
针对直接抽引飞管源头数据出现飞控计算机带负载能力较弱的问题,设计了非标422数字飞控总线采集系统。飞行试验结果表明,该系统工作性能稳定,运行安全、可靠。
a non-standard 422 digital flight control bus acquisition system was designed to solve the problem of weak load capacity of flight control computer due to the source data of direct pumping flight tube.The flight test results show that the system has stable performance,safe and reliable operation.
出处
《数码设计》
2019年第16期42-42,共1页
Peak Data Science
关键词
飞参记录器
飞控采集器
接口分配器
flight parameter recorder
Flight control collector
Interface distributor
