Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: Analytical synthesis

Abstract

The problem of stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle is solved analytically. The solution is based on the synthesis of output spectrum control of a MIMO system motion that uses a specially organized multilevel decomposition of the model of the dynamic system in the space of states. Results of numerical simulation are presented.