飞机刹车控制系统仿真测试平台设计  

Desigh of aircarft brake control system simulation test platform

作　　者：段栋栋[1] 骆德渊[1] 金伟[1] 付书阁[1] 

机构地区：[1]电子科技大学机械电子工程学院,四川成都611731

出　　处：《电子设计工程》2013年第9期131-133,共3页Electronic Design Engineering

摘　　要：针对飞机在地面的快速反应,安全升空和着陆能力,以及飞机刹车系统的性能等问题,将半实物仿真测试技术应用到飞机刹车系统中。建立实物与模型之间的关系,以LabWindows/CVI 2009为仿真开发平台,提出以实物代替模型引入仿真回路,与所建模型形成完整的飞机刹车半实物仿真系统的方法。结果表明:该测试系统与实物仿真相比投资少,效率高,同时又比传统数字仿真更接近实际,是理想的测试手段,为飞机刹车系统的实验研究提供了真实有效的实验平台。For the rapid response of the aircraft on the ground, safe launching and landing capability, as well as the performance of the aircraft brake system, the loop simulation test technology was applied to aircraft braking system. Establishing the relationship between the physical and the model which use LabWindows/CVI 2009 as simulation development platform, proposed the kind instead model introduced simulation loop, with the model form a complete the aircraft brake loop simulation system. The results show that the physical simulation of the test system with less investment, high efficiency, at the same time off than pure digital simulation more realistic which is the ideal means of testing. Providing a real and effective experimental platform to experimental study of aircraft braking systems.

关 键 词：刹车控制系统 LABWINDOWS CVI 仿真 测试系统 

分 类 号：TP216[自动化与计算机技术—检测技术与自动化装置]