NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Output Feedback M-MRAC Backstepping With Aerospace ApplicationsThe paper presents a certainty equivalence output feedback backstepping adaptive control design method for the systems of any relative degree with unmatched uncertainties without over-parametrization. It uses a fast prediction model to estimate the unknown parameters, which is independent of the control design. It is shown that the system's input and output tracking errors can be systematically decreased by the proper choice of the design parameters. The approach is applied to aerospace control problems and tested in numerical simulations.
Document ID
20140011532
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Stepanyan, Vahram
(California Univ. Santa Cruz, CA, United States)
Krishnakumar, Kalmanje Sriniva
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 10, 2014
Publication Date
January 13, 2014
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN12362
Report Number: ARC-E-DAA-TN12362
Meeting Information
Meeting: SciTech 2014
Location: National Harbor, MD
Country: United States
Start Date: January 13, 2014
End Date: January 17, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS2-03144
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Output feedback adaptive control
Unmatched uncertainties
Guaranteed transient performance
No Preview Available