摘要
依据高升力控制系统控制律以及系统软硬件平台,开发了高升力系统软件。针对驾驶员对手柄信号误操作的保护功能,提出了实时跟踪驾驶员控制指令的"矩阵跟踪法",增强了软件模块的内聚性,经综合仿真验证满足各项功能、性能指标,提高了软件控制精度,对后续其他型号类似软件设计具有一定的参考意义。
Using control law of high-lift control system and system software/hardware environment, high-lift control system software was developed . Aiming at preventing the system abnormality when pilots input incorrectly, a method“Matrix Track method”is presented, that protects the system by tracking pilot command in real-time , enhance software unit cohesion, and improve software control precision. Simulation synthesis proves that the software is able to meet the system’s functions and capabilities. The method also can be used for other types of airplanes.
出处
《航空科学技术》
2014年第3期31-34,共4页
Aeronautical Science & Technology
关键词
高升力控制系统
矩阵跟踪法
软件
high-lift control system
matrix track method
software
