飞机刹车系统方案设计及仿真分析  

Scheme Design and Simulation Analysis of Aircraft Brake System

作　　者：陶周亮[1] 聂宏[1,2] 魏小辉[1,2] 刘向尧[1] 尹乔之[1] 

机构地区：[1]南京航空航天大学机械结构力学及控制国家重点实验室,南京210016 [2]南京航空航天大学飞行器先进设计技术国防重点学科实验室,南京210016

出　　处：《航空工程进展》2013年第3期306-311,共6页Advances in Aeronautical Science and Engineering

基　　金：国家自然科学基金(51075203);江苏高校优势学科建设工程资助项目

摘　　要：构建飞机刹车系统方案设计环境,以提高飞机刹车系统方案设计阶段的设计效率和质量。研究刹车装置参数和防滑控制系统参数的快速确定方法,通过迭代的设计思想使结果符合设计要求;估算刹车装置性能和刹车系统的动态特性。在MATLAB/Simulink中建立刹车系统模型,通过MATLAB引擎调用的方式进行刹车系统的动力学分析;以某无人机刹车系统为设计实例进行其刹车系统的方案设计,动力学仿真中刹车系统工作良好,与实际工作状况基本吻合。结果表明:本文提供的飞机刹车方案设计方法快速有效。The aircraft brake system design environment is built to improve the scheme design efficiency and quality of aircraft brake. First, the brake system is designed according to the basic parameters of aircraft. Ac- cording to the parameters of brake device and anti-skid control system, the performance is estimated. Then, the model of brake system is built in MATLAB/Simulink and by using of MATLAB engine the dynamic analysis of the brake system is done. Finally, the design and dynamic simulation of an UAV brake system are accomplished as an example, and both of them coincide well with the actual working condition. Results show that the method of aircraft brake design presented in this paper is rapid and effective.

关 键 词：刹车系统 方案设计 性能估算 仿真分析 软件开发 

分 类 号：V226[航空宇航科学与技术—飞行器设计]