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该系统由计算机控制系统、数据采集系统、模拟闭环控制系统、执行系统等组成,直接用于验证新型飞机的强度设计是否成功。该系统成功地完成了全机悬空静力试验、机翼与前、后襟静力试验、起落架的单机或多机实时控制与采集疲劳试验等三个大型试验,并能实现多情况、多姿态、多谱型、多点协调加载和悬空姿态控制。试验证明该系统具有高精度和高可靠
The system consists of computer control system, data acquisition system, analog closed-loop control system, executive system and other components, directly used to verify the strength of the new aircraft design success. The system has successfully completed three large-scale experiments such as whole-body suspension static test, wing-front and back-lag static test, landing gear single-machine or multi-machine real-time control and acquisition fatigue test, Attitude, multi-spectrum, coordinated multi-point loading and dangling attitude control. Experiments show that the system has high precision and high reliability