JPL/波音陀螺仪驱动控制回路电子集成在自主鲁棒自定义可重构平台中的研究

E. F. Stefatos, T. Arslan, D. Keymeulen, I. Ferguson
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引用次数: 4

摘要

本文提出了一种用于喷气推进实验室/波音陀螺仪实现的自主架构。该体系结构的中心点是一个统一的可重构结构,它集成了两个定制的特别定制的可重构单元。前一种结构允许重新配置基于整数的计算,而后一种结构则处理那些需要小数精度的计算。该体系结构采用了许多其他技术,如原始算子和混合进化策略,以允许实时适应具有低功耗和高容错程度的高质量电路。仿真结果证明,在存在单硬误差的情况下,我们提出的架构能够在速度、精度和硬件利用率方面非常有效地适应高阶有限脉冲响应滤波器和比例积分控制器的功能。功耗分析表明我们的架构具有接近ASIC的性能
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Towards the Integration of Drive Control Loop Electronics of the JPL/Boeing Gyroscope within an Autonomous Robust Custom-Reconfigurable Platform
This paper presents an autonomous architecture for the implementation of the JPL/Boeing gyroscope. The central point of the architecture is a unified reconfigurable fabric, which integrates two custom especially tailored reconfigurable units. The former fabric enables the reconfiguration of integer based computations, whereas the later deals with those requiring fractional accuracy. The architecture employs a number of other techniques such as primitive operators and a hybrid evolutionary strategy in order to allow the real-time adaptation of high quality circuits with low power consumption and high degree of fault-tolerance. Simulation results prove that our proposed architecture is able to adapt, in the presence of single-hard-errors, the functionality of high-order finite-impulse-response filters and proportional-integral controllers very efficiently in terms of speed, accuracy and hardware utilization. Power analysis demonstrates the near ASIC performance of our architecture
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