NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Indirect Identification of Linear Stochastic Systems with Known Feedback DynamicsAn algorithm is presented for identifying a state-space model of linear stochastic systems operating under known feedback controller. In this algorithm, only the reference input and output of closed-loop data are required. No feedback signal needs to be recorded. The overall closed-loop system dynamics is first identified. Then a recursive formulation is derived to compute the open-loop plant dynamics from the identified closed-loop system dynamics and known feedback controller dynamics. The controller can be a dynamic or constant-gain full-state feedback controller. Numerical simulations and test data of a highly unstable large-gap magnetic suspension system are presented to demonstrate the feasibility of this indirect identification method.
Document ID
19970015306
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Huang, Jen-Kuang
(Old Dominion Univ. Norfolk, VA United States)
Hsiao, Min-Hung
(Taipei Inst. of Technology Taiwan, Province of China)
Cox, David E.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1996
Publication Information
Publication: Journal of Guidance, Control, and Dynamics
Publisher: American Inst. of Aeronautics and Astronautics, Inc.
Volume: 19
Issue: 4
Subject Category
Cybernetics
Report/Patent Number
NASA-CR-203237
NAS 1.26:203237
Report Number: NASA-CR-203237
Report Number: NAS 1.26:203237
Accession Number
97N18259
Funding Number(s)
CONTRACT_GRANT: NAS1-19858
CONTRACT_GRANT: NAG1-1056
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available