DocumentCode
2200913
Title
A minimalist hardware architecture for using commercial microcontrollers in space
Author
Caldwell, D.W. ; Rennels, D.A.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
1
fYear
1997
fDate
26-30 Oct 1997
Firstpage
5.2
Abstract
Microcontrollers provide very dense functionality for embedded applications ranging from telephones to automobiles. The acceptance of these devices for space applications has been hindered by their manufacture which often uses multiple semiconductor fabrication techniques and thereby compromises radiation tolerance. If such concerns could be mitigated, microcontrollers would provide substantial increase in performance for builders of spacecraft electronics. This paper presents hardware considerations for using commercial microcontrollers in space applications. The motivations for starting with commercial devices associated with their use are advantages of software versus hardware voting schemes to mitigate single-event effects are discussed. Interprocess communications approaches and schemes for improving I/O robustness are presented
Keywords
aerospace computing; built-in self test; computer architecture; fault tolerant computing; microcontrollers; reliability; special purpose computers; commercial microcontrollers; computational efficiency; computational errors; dense functionality; distributed functionality; embedded applications; minimalist hardware architecture; multiple semiconductor fabrication; radiation tolerance; self-checking; single-event effects; space applications; Aerospace electronics; Aircraft manufacture; Application software; Automobile manufacture; Fabrication; Hardware; Microcontrollers; Semiconductor device manufacture; Telephony; Voting;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1997. 16th DASC., AIAA/IEEE
Conference_Location
Irvine, CA
Print_ISBN
0-7803-4150-3
Type
conf
DOI
10.1109/DASC.1997.635091
Filename
635091
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