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Flight control system design factors for applying automated testing techniquesAutomated validation of flight-critical embedded systems is being done at ARC Dryden Flight Research Facility. The automated testing techniques are being used to perform closed-loop validation of man-rated flight control systems. The 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. Operationally applying automated testing techniques has accentuated flight control system features that either help or hinder the application of these techniques. The paper also discusses flight control system features which foster the use of automated testing techniques.
Document ID
19930021575
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sitz, Joel R. (NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Vernon, Todd H. (Planning Research Corp. Edwards, CA., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1990
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:4242
NASA-TM-4242
H-1631
Meeting Information
Meeting: Annual Digital Avionics System Conference
Location: Virginia Beach, VA
Country: United States
Start Date: October 15, 1990
End Date: October 18, 1990
Sponsors: IEEE
Accession Number
93N30764
Funding Number(s)
PROJECT: RTOP 533-02-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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