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Validation of the F-18 high alpha research vehicle flight control and avionics systems modificationsThe verification and validation process is a critical portion of the development of a flight system. Verification, the steps taken to assure the system meets the design specification, has become a reasonably understood and straightforward process. Validation is the method used to ensure that the system design meets the needs of the project. As systems become more integrated and more critical in their functions, the validation process becomes more complex and important. The tests, tools, and techniques which are being used for the validation of the high alpha research vehicle (HARV) turning vane control system (TVCS) are discussed and the problems and their solutions are documented. The emphasis of this paper is on the validation of integrated system.
Document ID
19900019226
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chacon, Vince
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Pahle, Joseph W.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Regenie, Victoria A.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1990
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1632
NAS 1.15:101723
NASA-TM-101723
Report Number: H-1632
Report Number: NAS 1.15:101723
Report Number: NASA-TM-101723
Meeting Information
Meeting: IEEE 9th Digital Avionics Systems Conference
Location: Virginia Beach, VA
Country: United States
Start Date: October 15, 1990
End Date: October 18, 1990
Accession Number
90N28542
Funding Number(s)
PROJECT: RTOP 505-68-71
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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