Nonlinearities in Landing Gear Model Incorporating Inerter

被引：0

作者：

Liu, Yuance ^{[1
]}

Chen, Michael Z. Q. ^{[1
]}

Tian, Yinan ^{[2
]}

机构：

[1] Univ Hong Kong, Dept Mech Engn, Hong Kong, Hong Kong, Peoples R China

[2] Nanjing Univ Sci & Technol, Sch Automat, Nanjing, Jiangsu, Peoples R China

来源：

2015 IEEE INTERNATIONAL CONFERENCE ON INFORMATION AND AUTOMATION | 2015年

关键词：

Nonlinearity; Inerter; Aircraft landing gear; Shimmy vibration; MECHANICAL NETWORKS;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

An inerter is a recently proposed two-node element in which the force across the two nodes is proportional to their relative acceleration. Studies based on linearization have previously been conducted on the application of inerters to landing gear for light civil aircraft to improve the resistance of such gear to shimmy vibration. Thus, the current research determines the effect of nonlinearities on the performance of the proposed model for aircraft landing gear in such vibration. This model is analyzed through a Simulink simulation, and conclusions are drawn on this effect and on the well-posedness of the linearized model.

引用

页码：696 / 701

页数：6

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