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Modeling and Experimental Efforts towards Robust Low-Cost Cruciform Canopy Control

机译:低成本低成本十字形机盖控制的建模和实验研究

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Over the years, precision guided cargo airdrop has taken many forms with most attempting to optimize payload delivery accuracy over all other variables. More recent developments have placed system cost and the ability to perform accurately in highly vertical drop environments as higher priorities, necessitating a departure from more traditional parafoil based vehicles. This work describes the numerical and experimental examination of a cruciform based cargo payload system in the context of modern operational considerations. The design process is holistic, making extensive use of a two-way fluid-structure interaction (FSI) model to characterize steady flight and coupling this with collection and analysis of tradition live drop test data to understand deployment dynamics and responses to environmental conditions. This has resulted in a system that has the potential to leverage existing concepts of operation and flight planning tools while extending operational and logistics support in real-world mission scenarios.
机译:多年来,精密引导的货物AITDOP已经采取了多种形式,最旨在优化所有其他变量的有效载荷传递精度。最近的发展已经放置了系统成本和能力在高度垂直的落下环境中表现为更高的优先级,所以需要出发更多传统的平板基车辆。这项工作描述了在现代操作考虑因素背景下的Cruciform基货有效载放系统的数值和实验检查。设计过程是整体的,使双向流体结构交互(FSI)模型广泛使用,以表征稳定飞行,并将其与传统实时跌幅测试数据的收集和分析进行耦合,以了解部署动态和对环境条件的响应。这导致了一个系统,有可能利用现有的运营和飞行计划工具概念,同时在现实世界的使命场景中延长运营和物流支持。

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