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Autonomous frequency domain identification: Theory and experimentThe analysis, design, and on-orbit tuning of robust controllers require more information about the plant than simply a nominal estimate of the plant transfer function. Information is also required concerning the uncertainty in the nominal estimate, or more generally, the identification of a model set within which the true plant is known to lie. The identification methodology that was developed and experimentally demonstrated makes use of a simple but useful characterization of the model uncertainty based on the output error. This is a characterization of the additive uncertainty in the plant model, which has found considerable use in many robust control analysis and synthesis techniques. The identification process is initiated by a stochastic input u which is applied to the plant p giving rise to the output. Spectral estimation (h = P sub uy/P sub uu) is used as an estimate of p and the model order is estimated using the produce moment matrix (PMM) method. A parametric model unit direction vector p is then determined by curve fitting the spectral estimate to a rational transfer function. The additive uncertainty delta sub m = p - unit direction vector p is then estimated by the cross spectral estimate delta = P sub ue/P sub uu where e = y - unit direction vectory y is the output error, and unit direction vector y = unit direction vector pu is the computed output of the parametric model subjected to the actual input u. The experimental results demonstrate the curve fitting algorithm produces the reduced-order plant model which minimizes the additive uncertainty. The nominal transfer function estimate unit direction vector p and the estimate delta of the additive uncertainty delta sub m are subsequently available to be used for optimization of robust controller performance and stability.
Document ID
19890016651
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yam, Yeung
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bayard, D. S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Hadaegh, F. Y.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mettler, E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Milman, M. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Scheid, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
April 15, 1989
Subject Category
Astronautics (General)
Report/Patent Number
NAS 1.26:184811
JPL-PUBL-89-8
NASA-CR-184811
Report Number: NAS 1.26:184811
Report Number: JPL-PUBL-89-8
Report Number: NASA-CR-184811
Accession Number
89N26022
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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