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Implementation and Evaluation of Multiple Adaptive Control Technologies for a Generic Transport Aircraft SimulationPresented here is the evaluation of multiple adaptive control technologies for a generic transport aircraft simulation. For this study, seven model reference adaptive control (MRAC) based technologies were considered. Each technology was integrated into an identical dynamic-inversion control architecture and tuned using a methodology based on metrics and specific design requirements. Simulation tests were then performed to evaluate each technology s sensitivity to time-delay, flight condition, model uncertainty, and artificially induced cross-coupling. The resulting robustness and performance characteristics were used to identify potential strengths, weaknesses, and integration challenges of the individual adaptive control technologies
Document ID
20100034875
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Campbell, Stefan F.
(NASA Ames Research Center Moffett Field, CA, United States)
Kaneshige, John T.
(NASA Ames Research Center Moffett Field, CA, United States)
Nguyen, Nhan T.
(NASA Ames Research Center Moffett Field, CA, United States)
Krishakumar, Kalmanje S.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 25, 2013
Publication Date
April 20, 2010
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN1569
Report Number: ARC-E-DAA-TN1569
Meeting Information
Meeting: Infotech@Aerospace
Location: Atlanta, GA
Country: United States
Start Date: April 20, 2010
End Date: April 22, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA08CG83C
Distribution Limits
Public
Copyright
Public Use Permitted.
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