Optymalizacja związków sprzężenia w automatycznym sterowaniu lotem

A concept of system optimization, which ensures the fastest damping of A. N. Golubyentsev's process for the linear n-th degree equations has been modified for the system described by matrix-vector equations The matrix form conditions enable the fast determination of suitable coefficients for the linear systems It is know that in the most of the cases the equations of controlled dynamic objects are presented in the form of a matrix set of equations. The modified method has been used for optimization of the stiffness and damping of the aircraf oscilations in the automatic flight control.