Optimal stabilization of the movement of an unmanned aerial vehicle with parametric uncertainty

Abstract

This article proposes a modal approach to the synthesis of robust systems for optimal stabilization of the program flight path of a UAV under conditions of uncertainty of its state parameters. The synthesis of a modal robust controller is implemented using the principle of guaranteed dynamics, which allows ensuring not only stability, but also the required quality of control. Ref. 14, pic. 1.

Keywords

• unmanned aerial vehicle
• uncertainty of parameters
• linear-quadratic optimization
• the principle of guaranteed dynamics
• modal synthesis