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The RTE inversion on FPGA aboard the Solar Orbiter PHI instrument

机译:Solar Orbiter PHI仪器上FPGA上的RTE反转

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In this work we propose a multiprocessor architecture to reach high performance in floating point operations by using radiation tolerant FPGA devices, and under narrow time and power constraints. This architecture is used in the PHI instrument that carries out the scientific analysis aboard the ESA's Solar Orbiter mission. The proposed architecture, in a SIMD flavor, is aimed to be an accelerator within the Data Processing Unit (it is composed by a main Leon processor and two FPGAs) for carrying out the RTE inversion on board the spacecraft using a relatively slow FPGA device -Xilinx XQR4VSX55-. The proposed architecture squeezes the FPGA resources in order to reach the computational requirements and improves the ground-based system performance based on commercial CPUs regarding time and power consumption. In this work we demonstrate the feasibility of using this FPGA devices embedded in the SO/PHI instrument. With that goal in mind, we perform tests to evaluate the scientific results and to measure the processing time and power consumption for carrying out the RTE inversion.
机译:在这项工作中,我们提出了一种多处理器体系结构,以通过使用耐辐射的FPGA器件并在狭窄的时间和功率约束下,在浮点运算中实现高性能。 PHI仪器中使用了这种体系结构,该仪器可对ESA的Solar Orbiter任务进行科学分析。拟议的架构具有SIMD风格,旨在成为数据处理单元(由一个主Leon处理器和两个FPGA组成)中的加速器,用于使用相对较慢的FPGA装置在航天器上进行RTE反转- Xilinx XQR4VS​​X55​​-。所提出的体系结构压缩了FPGA资源,以达到计算要求,并基于基于时间和功耗的商用CPU改进了基于地面的系统性能。在这项工作中,我们演示了使用嵌入在SO / PHI仪器中的FPGA器件的可行性。考虑到这一目标,我们进行测试以评估科学结果,并测量进行RTE反转的处理时间和功耗。

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