GOLGE: a case study of a secure data communication subsystem for micro-satellites

S. Yesil, R. Sever, B. Okcan, N. Ismailoglu
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引用次数: 5

Abstract

This paper presents a real-time data encryption/decryption subsystem developed for a satellite, which is planned to be launched in 2007 by TUBITAK-BILTEN. The subsystem GOLGE contains two ASICs, which perform encryption/decryption using AES (Advanced Encryption Standard) and RSA (Rivest-Shamir-Adleman) algorithms and a communication interface unit. The data/command interface of the GOLGE module is implemented on a reconfigurable ASIC (FPGA), where the encryption/decryption processors have previously been designed in TUBITAK-BILTEN and prototyped in ANTIS 0.35-/spl mu/m CMOS technology. The system uses an 8-bit bidirectional data bus, which operates at a maximum frequency of 40 MHz supplying a throughput of 160 Mbit/sec and a SpaceWire interface, which provides a 100 Mbit/sec serial data communication link.
微型卫星安全数据通信子系统的案例研究
本文介绍了为某卫星研制的实时数据加解密子系统,该子系统计划于2007年由TUBITAK-BILTEN公司发射。GOLGE子系统包含两个asic,使用AES(高级加密标准)和RSA (Rivest-Shamir-Adleman)算法和一个通信接口单元执行加密/解密。GOLGE模块的数据/命令接口在可重构ASIC (FPGA)上实现,其中加密/解密处理器先前已在TUBITAK-BILTEN中设计,并在ANTIS 0.35-/spl mu/m CMOS技术中进行原型设计。该系统使用8位双向数据总线,最大工作频率为40 MHz,提供160 Mbit/秒的吞吐量,SpaceWire接口提供100 Mbit/秒的串行数据通信链路。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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