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Case Study of Using High Performance Commercial Processors in Space
ISSN: 0148-7191, e-ISSN: 2688-3627
Published November 10, 2009 by SAE International in United States
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The purpose of the Space Shuttle Cockpit Avionics Upgrade project (1999 – 2004) was to reduce crew workload and improve situational awareness. The upgrade was to augment the Shuttle avionics system with new hardware and software. A major success of this project was the validation of the hardware architecture and software design. This was significant because the project incorporated new technology and approaches for the development of human rated space software. An early version of this system was tested at the Johnson Space Center for one month by teams of astronauts. The results were positive, but NASA eventually cancelled the project towards the end of the development cycle.
The goal to reduce crew workload and improve situational awareness resulted in the need for high performance Central Processing Units (CPUs). The choice of CPU selected was the PowerPC family, which is a reduced instruction set computer (RISC) known for its high performance. However, the requirement for radiation tolerance resulted in the re-evaluation of the selected family member of the PowerPC line. Radiation testing revealed that the original selected processor (PowerPC 7400) was too soft to meet mission objectives and an effort was established to perform trade studies and performance testing to determine a feasible candidate. At that time, the PowerPC RAD750s were radiation tolerant, but did not meet the required performance needs of the project. Thus, the final solution was to select the PowerPC 7455. This processor did not have a radiation tolerant version, but had some ability to detect failures. However, its cache tags did not provide parity and thus the project incorporated a software strategy to detect radiation failures. The strategy was to incorporate dual paths for software generating commands to the legacy Space Shuttle avionics to prevent failures due to the softness of the upgraded avionics.
|Journal Article||Challenges in Validating Safety-Critical Embedded Systems|
|Journal Article||Integrated Safety Management System|
|Technical Paper||Digital Optical Based Aircraft Actuator Controller Utilizing SiC Power Switches|
CitationFerguson, R. and Olivas, Z., "Case Study of Using High Performance Commercial Processors in Space," SAE Technical Paper 2009-01-3275, 2009, https://doi.org/10.4271/2009-01-3275.
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