航天器上的处理器

来自Jack's Lab
2014年1月9日 (四) 12:54Comcat (讨论 | 贡献)的版本

跳转到: 导航, 搜索

目录

1 概述

空间环境对电子信号的最大威胁就是电离辐射,其能使本来是1的数字信号“翻转”变成0,反之亦然

因此航天处理器的主要性能指标就是抗辐射性、容错性,还有就是可靠、稳定



2 SPARC



3 MIPS

3.1 Mongoose-V

Feature
        Radiation hardened
        10~15 MHz version of the MIPS R3000
        Developed by Synova, Inc.


Applications
  • NASA's Earth Observer 1 (EO-1) satellite (launched in Nov. 2000) --- Main flight computer
  • NASA's Microwave Anisotropy Probe (MAP), (launched in June 2001) --- Main flight computer similar to that on EO-1.
  • NASA's three microsatellites of Space Technology 5 (ST5) (launched in Mar. 2006) --- Onboard flight computer (the Command & Data Handling system)
  • NASA's New Horizons spacecraft --- Two computer system, the Command and Data Handling system and the Guidance and Control processor. Each of the two systems is duplicated for redundancy, giving a total of four computers.


Reference



3.2 RH32

Feature
        Radiation hardened, fault tolerance
        Based on MIPS R3000
        Manufactured by Honeywell


Applications


Reference



4 PowerPC

4.1 RHPPC

Feature
        Radiation hardened
        Based on PowerPC 603e, compatible with the PowerPC architecture (Book I-III)
        190MIPS @ 100MHz
        25 ~ 50 MHz 60xbus (SYSCLK)
        Superscalar, Out-of-order, 5 units (include a float point unit)
        Manufactured by Honeywell
Applications


Reference



4.2 RAD600



4.3 RAD750




5 C51



















个人工具
名字空间

变换
操作
导航
工具箱