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Dual adaptive control: Design principles and applicationsThe design of an actively adaptive dual controller based on an approximation of the stochastic dynamic programming equation for a multi-step horizon is presented. A dual controller that can enhance identification of the system while controlling it at the same time is derived for multi-dimensional problems. This dual controller uses sensitivity functions of the expected future cost with respect to the parameter uncertainties. A passively adaptive cautious controller and the actively adaptive dual controller are examined. In many instances, the cautious controller is seen to turn off while the latter avoids the turn-off of the control and the slow convergence of the parameter estimates, characteristic of the cautious controller. The algorithms have been applied to a multi-variable static model which represents a simplified linear version of the relationship between the vibration output and the higher harmonic control input for a helicopter. Monte Carlo comparisons based on parametric and nonparametric statistical analysis indicate the superiority of the dual controller over the baseline controller.
Document ID
19880018654
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Mookerjee, Purusottam
(Connecticut Univ. Storrs, CT, United States)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-177485
NAS 1.26:177485
Report Number: NASA-CR-177485
Report Number: NAS 1.26:177485
Accession Number
88N28038
Funding Number(s)
PROJECT: RTOP 505-61-51
CONTRACT_GRANT: NAG2-213
CONTRACT_GRANT: NAG2-318
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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