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Control Systems with Normalized and Covariance Adaptation by Optimal Control ModificationDisclosed is a novel adaptive control method and system called optimal control modification with normalization and covariance adjustment. The invention addresses specifically to current challenges with adaptive control in these areas: 1) persistent excitation, 2) complex nonlinear input-output mapping, 3) large inputs and persistent learning, and 4) the lack of stability analysis tools for certification. The invention has been subject to many simulations and flight testing. The results substantiate the effectiveness of the invention and demonstrate the technical feasibility for use in modern aircraft flight control systems.
Document ID
20160004241
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Nguyen, Nhan T.
Burken, John J.
Hanson, Curtis E.
Date Acquired
April 1, 2016
Publication Date
March 29, 2016
Subject Category
Cybernetics, Artificial Intelligence And Robotics
Aircraft Stability And Control
Report/Patent Number
Patent Number: US-Patent-9,296,474
Patent Application Number: US-Patent-Appl-SN-13/956,736
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,296,474
Patent Application
US-Patent-Appl-SN-13/956,736
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