Girija, G and Raol, JR (1993) Analysis of stabilised output error methods. Control Theory and Applications, IEE Proceedings, 143 (2). pp. 209-216. ISSN 1350-2379
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Abstract
In the paper, analysis of stabilised output-error methods (SOEMs) for parameter estimation of unstable aircraft is presented. These methods overcome the numerical difficulties encountered in parameter estimation of unstable systems by utilising measured states. The methods, along with the output error method and the equation error method, are briefly described for the sake of comparison. However, the main idea of the paper is to present asymptotic analysis of the SOEM. The results of application of SOEMs to simulated data of an unstable/augmented aircraft are presented
Item Type: | Article |
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Additional Information: | Copyright for this article belongs to IEE |
Uncontrolled Keywords: | Aircraft control;Asymptotic stability;Error analysis;Parameter estimation;Statistical analysis;Stabilised output error; Parameter estimation;Unstable aircraft;Equation error |
Subjects: | AERONAUTICS > Aircraft Stability and Control |
Depositing User: | MS Jayashree S |
Date Deposited: | 06 Feb 2008 |
Last Modified: | 07 Jun 2010 07:59 |
URI: | http://nal-ir.nal.res.in/id/eprint/4153 |
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