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- flight control with L1 adaptive control coverage of the flight envelope with a single design and
- parameter identification (PID) with an automated, efficient and accurate method for global aerodynamic modeling to enable rapid transition to flight with minimal initial knowledge of the vehicle dynamics.
Document ID
20200006108
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Date Acquired
May 13, 2020
Subject Category
Report/Patent Number
Meeting Information
Meeting: Aerospace Control and Guidance Systems Committee Meeting #110
Location: Auburn, ME
Country: US
Start Date: October 10, 2012
End Date: October 12, 2012
Sponsors: Langley Research Center
Funding Number(s)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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