Design of Nonlinear Control of Gas Turbine Engine Based on Constant Eigenvectors

A gas turbine engine represents a complex dynamic control object. Its characteristics change depending on the state of environment and regimes its operation. This paper discusses an algorithmic approach to design nonlinear controller, based concept constant eigenvectors analytical system. The proposed method makes it possible ensure stability required quality transient processes at different acceleration modes. In this case, constancy matrix canonical basis closed-loop system is assumed, which guarantees stability. neural network model approximator with one input multiple outputs considered. An example controller for considered, given in space. application approximation coefficients presented.