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Cooperative GN&C development in a rapid prototyping environmentThe Navigation, Control and Aeronautics Division (NCAD) at NASA-JSC is exploring ways of producing Guidance, Navigation and Control (GN&C) flight software faster, better, and cheaper. To achieve these goals NCAD established two hardware/software facilities that take an avionics design project from initial inception through high fidelity real-time hardware-in-the-loop testing. Commercially available software products are used to develop the GN&C algorithms in block diagram form and then automatically generate source code from these diagrams. A high fidelity real-time hardware-in-the-loop laboratory provides users with the capability to analyze mass memory usage within the targeted flight computer, verify hardware interfaces, conduct system level verification, performance, acceptance testing, as well as mission verification using reconfigurable and mission unique data. To evaluate these concepts and tools, NCAD embarked on a project to build a real-time 6 DOF simulation of the Soyuz Assured Crew Return Vehicle flight software. To date, a productivity increase of 185 percent has been seen over traditional NASA methods for developing flight software.
Document ID
19940034850
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bordano, Aldo
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Uhde-Lacovara, JO
(NASA Johnson Space Center Houston, TX, United States)
Devall, Ray
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Partin, Charles
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Sugano, Jeff
(Lockheed Engineering and Sciences Co. Houston, TX, United States)
Doane, Kent
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Compton, Jim
(McDonnell Douglas Aerospace Houston, TX, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computing in Aerospace Conference, 9th, San Diego, CA, Oct. 19-21, 1993, Technical Papers. Pt. 2 (A94-11401 01-62)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Computer Systems
Report/Patent Number
AIAA PAPER 93-4622
Accession Number
94A11505
Distribution Limits
Public
Copyright
Other

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