Analyses of Coupling Effect of Load Simulator of Aircraft Control Surface on Actuator Simulation Loop

摘要：

　　At present the design of the aircraft control surface simulator is all about how to eliminate the redundant moment and increase the tracking accuracy of load simulator.In this paper,for the abnormal phenomena appeared in the semi-physical simulation loop of the load simulator,a simulation analysis was made to illustrate that there is a strong coupling effect between the load simulator and the actuator simulation loop,and increasing the tracking accuracy of load simulator simply can not eliminate the effect on the semi-physical simulation system.Therefore,there are some limitations in the design of load simulator based on its performance indexes only.

关键词： load simulator semi-physical simulation coupling digital simulation

作者: Ju Tian Chengwei HU

作者单位: Guangzhou Civil Aviation College,Guangzhou GuangDong,China

会议类型: 国际会议

会议名称: 2012 International Conference on Intelligent System and Applied Material(2012智能系统与应用材料国际会议)(GSAM2012)

会议地点: 太原

会议语种:英文

页码: 912-915

在线出版日期: 2012-01-13（万方平台首次上网日期，不代表论文的发表时间）