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Software control and system configuration management: A systems-wide approachA comprehensive software control and system configuration management process for flight-crucial digital control systems of advanced aircraft has been developed and refined to insure efficient flight system development and safe flight operations. Because of the highly complex interactions among the hardware, software, and system elements of state-of-the-art digital flight control system designs, a systems-wide approach to configuration control and management has been used. Specific procedures are implemented to govern discrepancy reporting and reconciliation, software and hardware change control, systems verification and validation testing, and formal documentation requirements. An active and knowledgeable configuration control board reviews and approves all flight system configuration modifications and revalidation tests. This flexible process has proved effective during the development and flight testing of several research aircraft and remotely piloted research vehicles with digital flight control systems that ranged from relatively simple to highly complex, integrated mechanizations.
Document ID
19840023042
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Petersen, K. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Flores, C., Jr.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:85908
NASA-TM-85908
H-1256
Report Number: NAS 1.15:85908
Report Number: NASA-TM-85908
Report Number: H-1256
Meeting Information
Meeting: IEEE/AIAA 5th Digital Avionics Systems Conf.
Location: Seattle, WA
Country: United States
Start Date: October 31, 1983
End Date: November 3, 1983
Accession Number
84N31112
Funding Number(s)
PROJECT: RTOP 505-34-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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