摘要
介绍了飞机供电管理设备余度设计技术的发展,描述了某型飞机的三余度供电管理计算机构型设计和余度管理策略、同步及通信、表决机制以及系统验证方法。
The development of redundancy design technology of aircraft power supply management equipment is introduced, and the configuration design and redundancy management strategy, synchronization and eommuni- eation, and voting mechanism and system verification method of a tri-redundancy power supply management eomputer for a certain aircraft are described.
作者
李建勇
LI Jian-yong(AVIC Chengdu Kaitian Electronics Co.,Ltd.,Chengdu 610091,China)
出处
《测控技术》
CSCD
2018年第B11期350-353,386,共5页
Measurement & Control Technology
关键词
三余度
同步
CCDL
故障注入
tri-redundancy
synchronization
CCDL
fault injection