系统仿真学报 ›› 2017, Vol. 29 ›› Issue (10): 2518-2527.doi: 10.16182/j.issn1004731x.joss.201710036

• 仿真应用工程 • 上一篇    下一篇

某型飞机滑行转弯过程动态仿真分析

张谦1, 张颖姝2   

  1. 1.中航工业西安航空制动科技有限公司,陕西 西安 710075;
    2.西安交通大学,陕西 西安 710049
  • 收稿日期:2015-10-13 发布日期:2020-06-04
  • 作者简介:张谦(1968-),男,陕西韩城,博士,高工,研究方向为航空机轮刹车系统;张颖姝(1993-),女,陕西西安,学士,研究方向为系统控制与仿真。

Dynamic Simulation and Analysis of the Taxiing turning Process of Aircraft

Zhang Qian1, Zhang Yingshu2   

  1. 1. Management Department, AVIC Xi'an Aviation Brake Technology Co., Ltd., Xi'an 710075, China;
    2. Institute of Electronic and Information Engineering, Xi'an Jiaotong University, Xi'an 710049, China
  • Received:2015-10-13 Published:2020-06-04

摘要: 为了解决某型飞机存在的转弯困难问题,进行了差动刹车控制飞机作地面滑行转弯的动态仿真分析研究。通过对飞机转弯过程的分析,运用Matlab软件,在Simulink环境下进行了飞机地面滑行转弯过程的动态建模和仿真,研究得到了飞机差动转弯需求与机轮和刹车控制系统性能指标的对应关系。运用仿真的方法,复现了转弯困难故障,清楚了故障的机理,明确了改进工作的方向;研究结果同样对飞机转弯性能和起落架系统的总体设计具有重大的参考价值。

关键词: 飞机滑行转弯, 差动刹车, 动态仿真, 刹车系统

Abstract: To solvethe problem that a certain type of aircraft couldn't turn easily during taxiing,a research was carried out concerning the dynamic taxiing process simulation of the aircraft when only differential brake could be used for turning. After analyzing the aircraft turning process, and applying the software of Matlab, dynamic model of the turning process was established in the Simulink environment. After running the model, studying and analyzing the simulation results, the correspondence between the differential brake turning requirements and the performance of the wheel and brake control system was obtained. Usingthe simulation method,the turning difficult fault is reappeared,the mechanism of fault was clear, and the direction of the improvement was oriented. The researching result has great reference value for the aircraft turning performance and landing gear system entire designing..

Key words: aircraft taxiing turning, differential brake, dynamic simulation, brake system

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