On-Orbit Flight Results from the Reconfigurable Cibola Flight Experiment Satellite (CFESat)

被引：23

作者：

Caffrey, Michael ^{[1
]}

Morgan, Keith ^{[1
]}

Roussel-Dupre, Diane ^{[1
]}

Robinson, Scott ^{[1
]}

Nelson, Anthony ^{[1
]}

Salazar, Anthony ^{[1
]}

Wirthlin, Michael ^{[2
]}

Howes, William ^{[2
]}

Richins, Daniel ^{[2
]}

机构：

[1] Los Alamos Natl Lab, POB 1663, Los Alamos, NM 87545 USA

[2] Brigham Young Univ, NSF Ctr High Performance, Reconfigurable Computing CHREC, Dept Elect & Comp Engn, Provo, UT 84602 USA

来源：

PROCEEDINGS OF THE 2009 17TH IEEE SYMPOSIUM ON FIELD PROGRAMMABLE CUSTOM COMPUTING MACHINES | 2009年

基金：

美国国家科学基金会;

关键词：

FPGA; fault tolerant computing; configurable computing;

D O I：

10.1109/FCCM.2009.22

中图分类号：

TP3 [计算技术、计算机技术];

学科分类号：

0812 ;

摘要：

The Cibola Flight Experiment (CFE) is an experimental small satellite developed at the Los Alamos National Laboratory to demonstrate the feasibility of using FPGA-based reconfigurable computing for sensor processing in a space environment. The CFE satellite was launched on March 8, 2007 in low-earth orbit and has operated extremely well since its deployment. The nine Xilinx Virtex FPGAs used in the payload have been used for several high-throughput sensor processing applications and for single-event upset (SEU) monitoring and mitigation. This paper will describe the CFE system and summarize its operational results. In addition, this paper will describe the results from several SEU detection circuits that were performed on the spacecraft.

引用

页码：3 / +

页数：2

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