On correlation between the airport runway friction coefficient measurement results and the real-life aircraft take-off and landing braking Characteristics

V. Putov, A. Putov, V. Sheludko, V. P. Kazakov, A. Stotckaia, M. M. Kopichev, K. Ignatiev
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引用次数: 8

Abstract

In this paper it is considered the technique design and algorithms for friction testing measuring implementation that are based upon the simulation of the real aircraft breaking modes while takeoff and landing via the measuring wheel. Moreover, the design problem of the controlled electromechanical simulator of the measuring wheel braking modes for the towed measuring vehicle is considered and adequate model implementation for the increasing the efficiency of the measuring system that consider the resilient behavior of the pneumatic tire and gearing system of the towed vehicle, and non-linear Coulomb friction with Stribeck effect. Effectiveness increasing of the braking modes simulation is provided using the neuro fuzzy control system. Real aircraft braking modes' simulator will provide the friction measuring results that will correlate with the real-life aircraft braking modes' characteristics.
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机场跑道摩擦系数测量结果与实际飞机起降制动特性的相关性研究
本文研究了通过测量轮模拟真实飞机起降时的破碎模式,实现摩擦测试测量的技术设计和算法。在此基础上,研究了拖曳式测量车测轮制动模式受控机电模拟器的设计问题,并充分考虑了拖曳式测量车充气轮胎和传动系统的弹性特性以及非线性库仑摩擦与斯特里克效应的影响,为提高测量车的效率提供了充分的模型实现。利用神经模糊控制系统提高了制动模式仿真的有效性。真实飞机制动模式模拟器将提供与真实飞机制动模式特性相关的摩擦测量结果。
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