旋转前起落架摆振现象的数学分析

Ronald W. Beery
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引用次数: 6

摘要

给出了四自由度前起落架运动方程的推导。这些方程是利用强大的拉格朗日形式的一种特殊形式得到的。这种方法需要相对较少的物理直觉,并产生严格的结果。这种推导得到了非线性形式的运动微分方程,从而可以研究摆振幅度,以便合理设计阻尼装置。微分方程的线性化形式是与振幅无关的,这种关于摆振振幅的信息是不可能得到的。目前文献中只发现了线性化的微分方程。这里推导的线性化形式的运动方程与莫兰德发展的运动方程作了详细的比较,并讨论了这里所采用的形式主义所揭示的几个有趣的点。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Mathematical Analysis of Corotating Nose-Gear Shimmy Phenomenon
A derivation of the equation of motion of a nose gear having four degrees of freedom is presented. These equations are obtained by using a special form of the powerful Lagrangian formalism. This approach demands relatively little physical intuition and produces rigorous results. This derivation yields the differential equations of motion in their unlinearized form to make possible an investigation of shimmy amplitude for the proper design of damping devices. Such information about shimmy amplitude is not forthcoming from the linearized form of the differential equations, which are amplitude-independent. Only the linearized differential equations are at present found in the literature. A detailed comparison of the linearized form of the equations of motion here derived, with those developed by Moreland, is also presented with discussion of several points of interest revealed by the formalism here employed.
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