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Simulation Based Evaluation of Integrated Adaptive Control and Flight Planning TechnologiesThe objective of this work is to leverage NASA resources to enable effective evaluation of resilient aircraft technologies through simulation. This includes examining strengths and weaknesses of adaptive controllers, emergency flight planning algorithms, and flight envelope determination algorithms both individually and as an integrated package.
Document ID
20090028818
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Campbell, Stefan Forrest
(NASA Ames Research Center Moffett Field, CA, United States)
Kaneshige, John T.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
October 21, 2008
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN-213
Report Number: ARC-E-DAA-TN-213
Meeting Information
Meeting: Aviation Safety Conference
Location: Denver, CO
Country: United States
Start Date: October 21, 2008
Funding Number(s)
CONTRACT_GRANT: NNA04AA18B
Distribution Limits
Public
Copyright
Public Use Permitted.
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