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A New Approach to Aircraft Robust Performance AnalysisA recently developed algorithm for nonlinear system performance analysis has been applied to an F16 aircraft to begin evaluating the suitability of the method for aerospace problems. The algorithm has a potential to be much more efficient than the current methods in performance analysis for aircraft. This paper is the initial step in evaluating this potential.
Document ID
20040110938
Acquisition Source
Headquarters
Document Type
Other
Authors
Gregory, Irene M. (NASA Langley Research Center Hampton, VA, United States)
Tierno, Jorge E. (Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA-96-3860
Report Number: AIAA-96-3860
Distribution Limits
Public
Copyright
Public Use Permitted.

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