By Topic

Experimental validation of a performance model for a distributed recoverable Boeing 747 flight control system subject to digital upsets

Sign In

Cookies must be enabled to login.After enabling cookies , please use refresh or reload or ctrl+f5 on the browser for the login options.

Formats Non-Member Member
$31 $13
Learn how you can qualify for the best price for this item!
Become an IEEE Member or Subscribe to
IEEE Xplore for exclusive pricing!
close button

puzzle piece

IEEE membership options for an individual and IEEE Xplore subscriptions for an organization offer the most affordable access to essential journal articles, conference papers, standards, eBooks, and eLearning courses.

Learn more about:

IEEE membership

IEEE Xplore subscriptions

3 Author(s)
Rui Wang ; Dept. of Electr. & Comput. Eng., Old Dominion Univ., Norfolk, VA, USA ; Gray, W.S. ; Gonzalez, O.R.

This paper describes a High Intensity Radiated Fields experiment conducted at the NASA Langley Research Center to validate a tracking performance model for a Boeing 747 digital flight control system implemented on a distributed recoverable computing platform which is subject to upsets. While the upset data does not appear to be Markov, it is found that a burst model for the upset process can be introduced so that a Markov jump-linear performance model can reliably provide an upper bound on the tracking error of the system.

Published in:

System Theory (SSST), 2011 IEEE 43rd Southeastern Symposium on

Date of Conference:

14-16 March 2011