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Experimental Online Identification Of Aircraft Longitudinal Motion

Michal Dub, Rudolf Jalovecký

Abstract


This paper deals with current parameter identification principles used for a description of aircraft motion. Fundamental principles for an experimental online identification of difference state equation matrix coefficients are introduced. Then creation of a mathematical model using classic least squares method and usability of sequential least squares method for updating model parameters are described. The whole concept is tested with real measured data of the L-410 aircraft longitudinal motion using the software support of the MATLAB program.
Full paper

2006-12-15

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