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Aerospace Instrument-Making

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LINEAR MODEL MATRIX PARAMETERS ESTIMATION USING ADDITIONAL STATE VARIABLES
R.L. Leibov

This paper presents an aircraft turbofan engine multivariable linear model matrix parameters estimation in the time domain. The estimation makes use of linear model additional state variables those allow to diminish the difference between nonlinear and linear models. The linear model matrix elements are determined using nonlinear model time responses and nonlinear programming. The results of proposed linear model matrix elements estimation method application for aircraft turbofan engine operating point of minimal thrust are presented. Key words: linear model, matrix parameters, additional state variables, nonlinear programming, aircraft turbofan engine. E-mail: r_leibov@mtu_net.ru

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