Redhawk平台下飞机制动系统仿真研究  

Simulation of Aircraft Braking System Under Redhawk Platform

作　　者：刘丽卓[1] 谢利理[1] 李旭[1] 郑新华[1] 

机构地区：[1]西北工业大学自动化学院,陕西西安710129

出　　处：《测控技术》2015年第3期153-156,共4页Measurement & Control Technology

摘　　要：飞机制动系统的半物理仿真研究是提高飞机总体设计极为重要和有效的环节之一。以Redhawk并行仿真计算机为硬件平台,将刹车控制单元和液压模拟系统作为实物模型,在先进的Simulation Workbench(SWB)仿真环境下对飞机制动系统进行了半物理仿真研究。经仿真测试,该仿真系统设计合理、有效,能够满足飞机防滑制动系统性能的要求。该系统对构建高性能飞机防滑制动系统的研究具有工程实际意义。Hardware-in-the-loop simulation for the braking system of aircraft is one of the extremely important and effective link to improve aircraft design. Both anti-skid braking controller and hydraulic system being put into the hardware-in-the-loop simulation system which is based on Redhawk concurrent computer and Simula- tion Workbench for establishing braking system of aircraft. The test results show that the hardware-in-the-loop system established is practical and effective, in addition, this system has a strong significance on practical engi- neering and is helpful for the construction of high performance aircraft antiskid brake system.

关 键 词：飞机制动系统 Redhawk实时仿真机 半实物仿真 SWB 

分 类 号：V247.4[航空宇航科学与技术—飞行器设计]