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Validation through Full-Scale Flight ExplorationObjectives: a) Regain Stable Platform: 1) Metrics analogous to stability margins needed for adaptive control systems; 2) Avoid adverse structural interactions. b) Maneuverability: 1) Control vehicle within new constraints; 2) Respect structural limitations; 3) Inform pilot of new performance limitations. c) Provide ability to safely land airplane: 1) Develop safest recovery trajectory.
Document ID
20090040728
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Bosworth, John T.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 8, 2013
Publication Date
November 17, 2009
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-1078
Report Number: DFRC-1078
Meeting Information
Meeting: NASA Aviation Safety Technical Conference
Location: McLean, VA
Country: United States
Start Date: November 17, 2009
End Date: November 19, 2009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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