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A new Finite Element model of the SOFIA Primary Mirror Cell to investigate dynamical behavior

机译:SOFIA主镜单元的新有限元模型,用于研究动力学行为

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The telescope structure of the Stratospheric Observatory for Infrared Astronomy (SOFIA) is subject to vibration excitation due to aircraft motions and turbulence from the airflow coming into the telescope cavity. A proper understanding of the dynamical behavior of the telescope structure under operational loads is crucial for pointing control and measures against higher order optical aberrations. During design and construction a Finite Element model of the telescope assembly has been created in order to assess the structural integrity and the early performance. This legacy model used conservative assumptions and had a coarse approach on the approximation of some structural features. We present an updated Finite Element model of the SOFIA Primary Mirror Assembly, which represents support members as well as the primary mirror itself in greater detail, in order to support ongoing development for performance optimization. An iterative approach employing structural optimization was used to tune the model in order to fit modal parameters of the Primary Mirror Assembly which were measured in a test campaign prior to integration into the full telescope structure. The updated and tuned model is used to calculate deformations due to gravity, thermal loads and dynamic excitation. These deformations serve as input for ray-tracing analyses to investigate alterations in the light path in order to evaluate pointing errors and higher order optical aberrations.
机译:由于飞机运动和来自进入望远镜腔的气流的湍流,红外平流层红外天文台(SOFIA)的望远镜结构容易受到振动的激励。正确理解望远镜结构在工作负载下的动力学行为对于指向控制和针对更高阶光学像差的措施至关重要。在设计和建造过程中,已经创建了望远镜组件的有限元模型,以评估结构完整性和早期性能。这个传统模型使用保守的假设,并对某些结构特征进行了粗略的处理。我们提供了SOFIA主镜组件的更新的有限元模型,该模型更详细地表示了支持成员以及主镜本身,以支持进行中的性能优化开发。为了适应主镜组件的模态参数,使用了一种采用结构优化的迭代方法来调整模型,以在集成到完整的望远镜结构之前的测试活动中对其进行测量。更新和调整后的模型用于计算由于重力,热负荷和动态激励引起的变形。这些变形用作光线跟踪分析的输入,以研究光路的变化,以便评估指向误差和高阶光学像差。

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