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Developments in optimized load calculation and extreme load detection: summary of EADS-CASA's main static loads activities in CleanSky Smart Fixed Wing Aircraft, work package on Advanced Loads Control Techniques

机译:优化负荷计算和极限负荷检测方面的发展:EADS-CASA在CleanSky智能固定翼飞机中的主要静态负荷活动摘要,有关先进负荷控制技术的工作包

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EADS-CASA's Static Loads Domain participated of the Clean Sky initiative developing several activities targeting the improvement of the available static loads calculation methodologies within the work package on Advanced Loads Control Techniques of the CleanSky Smart Fixed Wing Aircraft project. This paper summarizes the progress made in the two most relevant activities, namely the optimized preliminary load calculation method, also known as aircraft response confinement method, and the extreme load detection method. The first methodology targets the calculation of design loads by means of constrained optimization performed on the loads model, and has shown to be a quick but highly conservative methodology. The second method tries to reduce the number of maneuver simulations by means of optimal case selection, and has shown to be a very powerful and efficient tool.
机译:EADS-CASA的“静载荷领域”参加了“清洁天空”倡议,该组织开展了多项活动,旨在改善“清洁天空”智能固定翼飞机项目的“先进载荷控制技术”工作包中的可用静载荷计算方法。本文总结了两个最相关活动的进展,即优化的初步负荷计算方法(也称为飞机响应限制方法)和极限负荷检测方法。第一种方法论是通过对载荷模型进行约束优化来设计载荷的计算,并且已经证明是一种快速但高度保守的方法论。第二种方法试图通过优化案例选择来减少机动仿真的次数,并且已经证明是一种非常强大和有效的工具。

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