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Mitigation of Thermo-cycling effects in Flip-chip FPGA-based Space-borne Systems by Cyclic On-chip Task Relocation

机译:通过循环片上任务重定位减轻基于倒装芯片的基于FPGA的航天系统中的热循环效应

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Thermal cycling is one of the major factors that influences aging, failure and thus, thereliability of FPGA-based systems deployed on spacecrafts performing orbital missions. Circularmotion of the spacecrafts around the Earth or other planets causes significant variations of temperature in their electronic systems, resulting in thermo-cycling. For FPGA-based systems, thermal cycling depends on: off-board temperature variations, power dissipation of on-board components and on-chip temperature variations. The on-chip level of the system utilizing flip-chip FPGAs is the most sensitive to thermo-cycling. This paper presents a method for mitigating the thermo-cycling effects on flip-chip FPGAs. It is based on cyclically relocating tasks with high power dissipation to regions where tasks with low power emission are allocated and vice-versa. The cycle period depends on the difference between clock frequencies associated with thetasks and area occupied by the task circuits. The proposed approach utilizes the experimental results gained on the Xilinx 7000 series FPGA, Zynq-7020. It was determined that control of relocation cycle can keep the dynamics of temperature variations on the board and chip level coherent and thus can minimize the thermo-cycling effect on FPGA-based space-borne computing platforms.
机译:热循环是影响老化,故障以及影响部署在执行轨道任务的航天器上的基于FPGA的系统的可靠性的主要因素之一。航天器绕地球或其他行星的圆周运动会导致其电子系统的温度发生明显变化,从而导致热循环。对于基于FPGA的系统,热循环取决于:板外温度变化,板载组件的功耗以及芯片上温度变化。使用倒装芯片FPGA的系统的片上级别对热循环最敏感。本文提出了一种减轻倒装芯片FPGA上热循环效应的方法。它基于将具有高功耗的任务周期性地重新分配到分配了低功耗任务的区域,反之亦然。周期取决于与任务相关的时钟频率与任务电路占用的面积之间的差异。所提出的方法利用了在Xilinx 7000系列FPGA Zynq-7020上获得的实验结果。可以确定的是,对重定位周期的控制可以使电路板和芯片级温度变化的动态保持一致,从而可以将对基于FPGA的星载计算平台的热循环影响降至最低。

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