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Peak-Seeking Control Using Gradient and Hessian EstimatesA peak-seeking control method is presented which utilizes a linear time-varying Kalman filter. Performance function coordinate and magnitude measurements are used by the Kalman filter to estimate the gradient and Hessian of the performance function. The gradient and Hessian are used to command the system toward a local extremum. The method is naturally applied to multiple-input multiple-output systems. Applications of this technique to a single-input single-output example and a two-input one-output example are presented.
Document ID
20100024511
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Ryan, John J.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Speyer, Jason L.
(California Univ. Los Angeles, CA, United States)
Date Acquired
August 24, 2013
Publication Date
June 30, 2010
Subject Category
Aerodynamics
Report/Patent Number
DFRC-1062
DFRC-E-DAA-TN1838
Report Number: DFRC-1062
Report Number: DFRC-E-DAA-TN1838
Meeting Information
Meeting: 2010 American ControI Conference - ACC2010
Location: Baltimore, MD
Country: United States
Start Date: June 30, 2010
End Date: July 2, 2010
Distribution Limits
Public
Copyright
Public Use Permitted.
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