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Virtual Air Data System Architecture for Space Reentry Applications

机译:用于太空再入应用的虚拟空中数据系统架构

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In this paper, an advanced air data system architecture based on the concept of virtual air data is proposed. Virtualnair data are virtual measurements based on the combination of inertial measurements with weather forecast datancoming from a meteorological model. This model can be considered as a virtual sensor that provides information onnwind velocities, air temperature, and air pressure. The combination of inertial measurements with weather forecastndata has been carried out using a sensor fusion algorithm (specifically, an extended Kalman filter) allowing thenestimation of the true-air-speed components. This kind of air data system architecture allows most of the typicalnlimitations of conventional air data probes to be overcome and does not require any specific experimental orncomputational fluid dynamics calibration campaign or any thermal protection system when dealing with reentrynapplications. Its effectiveness has been demonstrated with two practical applications, the first based on the postflightnanalysis of the first Dropped Transonic Flight Test mission (carried out by the Italian Aerospace Research Center)nand the second based on a simulated case of the second Dropped Transonic Flight Test planned for the next years.
机译:本文提出了一种基于虚拟航空数据概念的先进航空数据系统架构。虚拟航空数据是基于惯性测量与来自气象模型的天气预报数据相结合的虚拟测量。该模型可以视为提供有关风速,气温和气压信息的虚拟传感器。惯性测量与天气预报数据的结合已经使用允许融合真实风速分量的传感器融合算法(特别是扩展的卡尔曼滤波器)进行了。这种空气数据系统架构可以克服常规空气数据探头的大多数典型局限性,并且在处理再入应用时不需要任何特定的实验或计算流体动力学校准活动或任何热保护系统。它的有效性已在两个实际应用中得到了证明,第一个基于对首次降落式超音速飞行测试任务(由意大利航空航天研究中心进行)的飞行后分析,第二个基于计划中的第二个降落式超音速飞行测试的模拟案例接下来的几年。

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