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Alternating Between Software Models and Real Hardware in the System Integration Lab for theIncremental Development of the Space Launch System Program Avionics
The MSFC System Integration Lab (SIL) supports avionics development of NASA’s Space Launch System—a new U.S. heavy-lift launch vehicle for NASA’s next generation of human space exploration beyond low-Earth orbit. The SIL facility allows for the incremental development of system components by either hosting real hardware in the loop and/or software models of those components. Through this functionality test teams are able to evaluate overall system performance as components are designed, built and modified.

Early hardware/software integration and testing reduces risks and saves overall cost and schedule throughout a program/project life cycle. By performing early hardware/software integration, potential architecture and interface-related problems can be identified, and thus reduce associated risk as early in the design cycle as possible when problems are the least expensive to resolve while also improving the design and requirements. This presentation will illustrate the power of employing a hardware in the loop simulation system for the development of novel spacecraft avionics.

Document ID
20205007078
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Matthew Pickard
(University of Alabama in Huntsville Huntsville, Alabama, United States)
Aaron Itzkovitz
(ESSCA)
Date Acquired
September 1, 2020
Subject Category
Launch Vehicles And Launch Operations
Meeting Information
Meeting: AIAA Next Gen Symposium
Location: Virtual
Country: US
Start Date: October 22, 2020
End Date: October 24, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
TASK: ES53.03.01.SSEI.AB1.02
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Space Launch System
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