Dynamic analysis of airships with small deformations

N. Azouz, Y. Bestaoui, O. Lemaître
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引用次数: 11

Abstract

The theory of modelling and control of airships was mostly imported from the fields of science and engineering of underwater vehicles. However the main hypothesis of rigidity of the structure may be improved to take into account the flexibility of the hull of an airship. We present an approach for analysing dynamic elastic deformable airships in an ideal fluid. Our model uses the updated Lagrangian method in combination with a large displacement and small deformation (Green) strain tensor formulation. Analogy is made with classical structural dynamics. The description of the behaviour of the airship consists of a continuous differential equation that is solved using a Rayleigh-Ritz technique combined with the finite element method. The method proposes also to take into account the coupling between the rigid body motion and the deformation as well as the interaction and coupling with the fluid surrounding.
小变形飞艇的动力学分析
飞艇的建模和控制理论主要是从水下航行器的科学和工程领域引进的。然而,考虑到飞艇船体的柔韧性,可以改进结构刚度的主要假设。提出了一种分析理想流体中动态弹性可变形飞艇的方法。我们的模型使用更新的拉格朗日方法结合大位移和小变形(格林)应变张量公式。与经典结构动力学作了类比。飞艇的行为描述由一个连续微分方程组成,该方程采用瑞利-里兹技术结合有限元法求解。该方法还考虑了刚体运动与变形之间的耦合以及与周围流体的相互作用和耦合。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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