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NASA TSRV essential flight control system requirements via object oriented analysisThe objective was to analyze the baseline flight control system of the Transport Systems Research Vehicle (TSRV) and to develop a system specification that offers high visibility of the essential system requirements in order to facilitate the future development of alternate, more advanced software architectures. The flight control system is defined to be the baseline software for the TSRV research flight deck, including all navigation, guidance, and control functions, and primary pilot displays. The Object Oriented Analysis (OOA) methodology developed is used to develop a system requirement definition. The scope of the requirements definition contained herein is limited to a portion of the Flight Management/Flight Control computer functionality. The development of a partial system requirements definition is documented, and includes a discussion of the tasks required to increase the scope of the requirements definition and recommendations for follow-on research.
Document ID
19920010257
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Duffy, Keith S.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Hoza, Bradley J.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1992
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.26:189573
NASA-CR-189573
Report Number: NAS 1.26:189573
Report Number: NASA-CR-189573
Accession Number
92N19499
Funding Number(s)
CONTRACT_GRANT: NAS1-18027
PROJECT: RTOP 505-66-41-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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