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State-space self-tuner for on-line adaptive controlDynamic systems, such as flight vehicles, satellites and space stations, operating in real environments, constantly face parameter and/or structural variations owing to nonlinear behavior of actuators, failure of sensors, changes in operating conditions, disturbances acting on the system, etc. In the past three decades, adaptive control has been shown to be effective in dealing with dynamic systems in the presence of parameter uncertainties, structural perturbations, random disturbances and environmental variations. Among the existing adaptive control methodologies, the state-space self-tuning control methods, initially proposed by us, are shown to be effective in designing advanced adaptive controllers for multivariable systems. In our approaches, we have embedded the standard Kalman state-estimation algorithm into an online parameter estimation algorithm. Thus, the advanced state-feedback controllers can be easily established for digital adaptive control of continuous-time stochastic multivariable systems. A state-space self-tuner for a general multivariable stochastic system has been developed and successfully applied to the space station for on-line adaptive control. Also, a technique for multistage design of an optimal momentum management controller for the space station has been developed and reported in. Moreover, we have successfully developed various digital redesign techniques which can convert a continuous-time controller to an equivalent digital controller. As a result, the expensive and unreliable continuous-time controller can be implemented using low-cost and high performance microprocessors. Recently, we have developed a new hybrid state-space self tuner using a new dual-rate sampling scheme for on-line adaptive control of continuous-time uncertain systems.
Document ID
19940028437
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Shieh, L. S.
(Houston Univ. TX, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Cybernetics
Report/Patent Number
NASA-CR-195836
NAS 1.26:195836
Report Number: NASA-CR-195836
Report Number: NAS 1.26:195836
Accession Number
94N32943
Funding Number(s)
CONTRACT_GRANT: NAG9-380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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