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Flight control system design factors for applying automated testing techniquesThe principal design features and operational experiences of the X-29 forward-swept-wing aircraft and F-18 high alpha research vehicle (HARV) automated test systems are discussed. It is noted that operational experiences in developing and using these automated testing techniques have highlighted the need for incorporating target system features to improve testability. Improved target system testability can be accomplished with the addition of nonreal-time and real-time features. Online access to target system implementation details, unobtrusive real-time access to internal user-selectable variables, and proper software instrumentation are all desirable features of the target system. Also, test system and target system design issues must be addressed during the early stages of the target system development. Processing speeds of up to 20 million instructions/s and the development of high-bandwidth reflective memory systems have improved the ability to integrate the target system and test system for the application of automated testing techniques. It is concluded that new methods of designing testability into the target systems are required.
Document ID
19910069987
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sitz, Joel R.
(NASA Flight Research Center Edwards, CA, United States)
Vernon, Todd H.
(Planning Research Corp. 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
Location: Virginia Beach, VA
Country: United States
Start Date: October 15, 1990
End Date: October 18, 1990
Accession Number
91A54610
Distribution Limits
Public
Copyright
Other

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