摘要
论述了高升力控制系统的功能、组成和工作原理。分析了新一代航空电子系统的发展方向和多信息综合化的设计思想。设计了高升力控制系统核心控制计算机的总体结构，获取并综合了传感器信息、作动器信息以及相关联的飞机其它系统信息。分析了多设备协同管理条件下的系统状态关系，设计了系统多状态的管理功能。分析了控制器和作动器的多余度通道控制模式，设计了多设备的协同任务控制功能。
The composition, functions and operating principles of the high lift control system are discussed. The development direction of the new generation avionics system and the multi-information synthesis design ideas are analyzed. The overall structure of the core computer with high lift control system is designed for acquiring and integration of sensor information, actuator information and other related aircraft system information. System state relationship under the condition of multi-device cooperative management is analyzed and the system management function is designed in different states. Finally redundancy channel control mode of controller and actuator is analyzed. Based on this, the cooperative task control function of multi-device is designed.
作者
李育
李婷
李欣
LI Yu;LI Ting;LI Xin(AVIC The First Aircraft Institute, Xi＇an 710089, China)
出处
《航空电子技术》
2018年第A01期108-112,共5页
Avionics Technology
关键词
数据融合
多信息综合
状态管理
航空机载软件
高升力控制
data fusion
multi information synthesis
state management
aviation airborne software
high lift control
