DocumentCode :
2838829
Title :
Case study of the Space Shuttle cockpit avionics upgrade software
Author :
Ferguson, Roscoe C. ; Thompson, Hiram C.
Author_Institution :
United Space Alliance LLC, Houston, TX, USA
Volume :
2
fYear :
2005
fDate :
30 Oct.-3 Nov. 2005
Abstract :
The purpose of the Space Shuttle Cockpit Avionics Upgrade project was to reduce crew workload and improve situational awareness. The upgrade was to augment the Shuttle avionics system with new hardware and software. An early version of this system was used to gather human factor statistics in the Space Shuttle Motion Simulator of the Johnson Space Center for one month by multiple teams of astronauts. The results were compiled by NASA Ames Research Center and it was determined that the system provided a better than expected increase in situational awareness and reduction in crew workload. Even with all of the benefits of the system, NASA cancelled the project towards the end of the development cycle. 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. This paper serves as a case study to document knowledge gained and techniques that can be applied for future space avionics development efforts. The major technological advances were the use of reflective memory concepts for data acquisition and the incorporation of Commercial off the Shelf (COTS) products in a human rated space avionics system. The infused COTS products included a real time operating system, a resident linker and loader, a display generation tool set, and a network data manager. Some of the successful design concepts were the engineering of identical outputs in multiple avionics boxes using an event driven approach and inter-computer communication, a reconfigurable data acquisition engine, the use of dynamic linking at runtime, and the use of a dynamic bus bandwidth allocation algorithm. Other significant experiences captured were the use of prototyping to reduce risk, and the correct balance between Object Oriented and Functional based programming.
Keywords :
aerospace computing; avionics; data acquisition; functional programming; hardware-software codesign; object-oriented programming; reconfigurable architectures; space vehicle electronics; Space Shuttle cockpit avionics; crew workload; dynamic bus bandwidth allocation algorithm; functional based programming; hardware architecture; human factor statistics; human rated space avionics system; intercomputer communication; object oriented programming; reconfigurable data acquisition engine; runtime dynamic linking; situational awareness; software design; Aerospace electronics; Computer architecture; Data acquisition; Hardware; Human factors; NASA; Object oriented modeling; Space shuttles; Space technology; Statistics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Digital Avionics Systems Conference, 2005. DASC 2005. The 24th
Print_ISBN :
0-7803-9307-4
Type :
conf
DOI :
10.1109/DASC.2005.1563454
Filename :
1563454
Link To Document :
بازگشت