On-Board Partial Run-Time Reconfiguration for Pico-Satellite Constellations

T. Vladimirova, Xiaofeng Wu
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引用次数: 18

Abstract

Distributed satellite systems are considered a promising new direction in spacecraft architecture design. Pico-satellite constellations flying in low Earth orbit (LEO) could become an efficient and low-cost solution to Earth observation and remote sensing in the future. There is a pressing need for condition-based maintenance, self-repair and upgrade capabilities on-board satellites in order to enable future space applications. In this paper we present a methodology for onboard partial run-time reconfiguration to enable onboard system-level functional changes ensuring correct operation, longer life and higher quality of service. The technique of partial run-time reconfiguration is introduced and a remote reconfiguration methodology is described. The architecture of an FPGA-based reconfigurable SoC design for on-board computing is outlined. A case study, which demonstrates the feasibility of the approach, is presented
微型卫星星座的星上部分运行时重构
分布式卫星系统被认为是航天器结构设计的一个有前途的新方向。在低地球轨道上飞行的微型卫星星座可能成为未来地球观测和遥感的一种高效、低成本的解决方案。迫切需要对卫星进行基于状态的维护、自我修复和升级能力,以便使未来的空间应用成为可能。在本文中,我们提出了一种车载部分运行时重新配置的方法,以实现车载系统级功能更改,确保正确运行,延长使用寿命和提高服务质量。介绍了部分运行时重构技术,并描述了一种远程重构方法。概述了一种基于fpga的可重构板载SoC设计体系结构。最后给出了一个实例,验证了该方法的可行性
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