Computational Homogenization for Inverse Design of Surface-based Inflatables

IF 7.8 1区 计算机科学 Q1 COMPUTER SCIENCE, SOFTWARE ENGINEERING
Y. Ren, Julian Panetta, Seiichi Suzuki, Uday Kusupati, Florin Isvoranu, Mark Pauly
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Abstract

Surface-based inflatables are composed of two thin layers of nearly inextensible sheet material joined together along carefully selected fusing curves. During inflation, pressure forces separate the two sheets to maximize the enclosed volume. The fusing curves restrict this expansion, leading to a spatially varying in-plane contraction and hence metric frustration. The inflated structure settles into a 3D equilibrium that balances pressure forces with the internal elastic forces of the sheets. We present a computational framework for analyzing and designing surface-based inflatable structures with arbitrary fusing patterns. Our approach employs numerical homogenization to characterize the behavior of parametric families of periodic inflatable patch geometries, which can then be combined to tessellate the sheet with smoothly varying patterns. We propose a novel parametrization of the underlying deformation space that allows accurate, efficient, and systematical analysis of the stretching and bending behavior of inflated patches with potentially open boundaries. We apply our homogenization algorithm to create a database of geometrically diverse fusing patterns spanning a wide range of material properties and deformation characteristics. This database is employed in an inverse design algorithm that solves for fusing curves to best approximate a given input target surface. Local patches are selected and blended to form a global network of curves based on a geometric flattening algorithm. These fusing curves are then further optimized to minimize the distance of the deployed structure to target surface. We show that this approach offers greater flexibility to approximate given target geometries compared to previous work while significantly improving structural performance.
基于表面的充气艇逆向设计的计算同质化
基于表面的充气艇由两层薄薄的几乎不可拉伸的片状材料组成,并沿着精心选择的融合曲线连接在一起。在充气过程中,压力会将两层薄片分开,以最大限度地增加封闭体积。熔合曲线限制了这种膨胀,导致平面内收缩的空间变化,从而产生度量失真。膨胀后的结构会进入三维平衡状态,平衡压力力和薄片的内部弹性力。我们提出了一个计算框架,用于分析和设计具有任意融合模式的基于表面的充气结构。我们的方法采用数值均质化来表征周期性充气贴片几何参数族的行为,然后将其结合起来,以平滑变化的模式对薄片进行细分。我们提出了一种新颖的底层变形空间参数化方法,可以准确、高效、系统地分析具有潜在开放边界的充气贴片的拉伸和弯曲行为。我们应用我们的均质化算法创建了一个包含多种几何融合图案的数据库,涵盖了广泛的材料特性和变形特征。该数据库可用于逆向设计算法,该算法可求解融合曲线,以最接近给定的输入目标表面。根据几何扁平化算法,选择并混合局部斑块,形成全局曲线网络。然后进一步优化这些融合曲线,使部署结构与目标表面的距离最小。我们的研究表明,与之前的研究相比,这种方法在近似给定目标几何形状方面具有更大的灵活性,同时还能显著提高结构性能。
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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来源期刊
ACM Transactions on Graphics
ACM Transactions on Graphics 工程技术-计算机:软件工程
CiteScore
14.30
自引率
25.80%
发文量
193
审稿时长
12 months
期刊介绍: ACM Transactions on Graphics (TOG) is a peer-reviewed scientific journal that aims to disseminate the latest findings of note in the field of computer graphics. It has been published since 1982 by the Association for Computing Machinery. Starting in 2003, all papers accepted for presentation at the annual SIGGRAPH conference are printed in a special summer issue of the journal.
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