飞机作动筒耐久循环加载试验计算机控制系统设计

Design of Computer Control System for Endurance Cycle Loading Test of Aircraft Actuating Cylinder

介绍某飞机作动筒耐久循环试验电液伺服加载控制系统的设计。该控制系统以工控机为核心，实时完成载荷谱的分解计算、控制信号校正、试验数据的采集和处理。

This paper introduces the design of electrohydraulic servo control syatm for endurance cycle test of some aircraft actuating cylinder. This control system takes the operating control as core to complete replving calculation of load spectrum,correction of contral signal and acquisition and processing of test data in real time.