摘要
为了满足民用飞机刹车控制律半物理试验中各种试验工况要求,本文研究了一种专用试验测试系统,该系统既有通用数据采集系统的通用性和多功能性,又能够满足飞机刹车系统特性参数测试的专有性要求,架构简单,且系统可靠、稳定,很好的满足了刹车控制律的试验需求。
In order to meet the requirements of various test conditions,a test system was studied,which not only had the versatility and multi-functionality of the general data acquisition system,but also can meet the exclusive requirements of the characteristic parameter test of the aircraft brake system.The architecture was simple,and the system was reliable and stable,which would meet the test requirements of the brake control algorithm.
作者
李雪松
LI Xue-song(State Key Laboratory of Airliner Integration Technology and Flight Simulation,Shanghai Aircraft Design and Research Institute,Shanghai 201210)
出处
《航空精密制造技术》
2024年第3期47-48,54,共3页
Aviation Precision Manufacturing Technology