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 valve control system (TVCS) are discussed, and their solutions are documented. The emphasis of this paper is on the validation of integrated systems.
Document ID
19910069954
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 Flight Research Center Edwards, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: IEEE/AIAA/NASA Digital Avionics Systems Conference