The optimization of the lateral motion control system of an unmanned aerial vehicle

Abstract

The article is devoted to the possibility of constructing an aircraft lateral motion control system only using the rudder; a mathematical model of such a system is obtained based on the structuring of an unmanned aerial vehicle model. The design of optimal lateral motion control of a UAV is carried out using the linear-quadratic optimization method in the complex domain for single-control systems. As an optimization criterion, a quadratic criterion in the form of restrictions on the control energy is used. Examples of system modeling are given.