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Rapid Automated Aircraft Simulation Model Updating from Flight Data

Author
Morelli, Eugene A.
Published
February 28, 2011.
Physical Description
1 electronic document
Additional Creators
Brian, Geoff
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Techniques to identify aircraft aerodynamic characteristics from flight measurements and compute corrections to an existing simulation model of a research aircraft were investigated. The purpose of the research was to develop a process enabling rapid automated updating of aircraft simulation models using flight data and apply this capability to all flight regimes, including flight envelope extremes. The process presented has the potential to improve the efficiency of envelope expansion flight testing, revision of control system properties, and the development of high-fidelity simulators for pilot training.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20110009996.
NF1676L-11838.
14th Australian International Aerospace Congress(AIAC14-AERO); 28 Feb. - 3 Mar. 2011; Melbourne; Australia.
Terms of Use and Reproduction
Copyright, Distribution as joint owner in the copyright.
View MARC record | catkey: 15991372