HANDLING DYNAMIC NONLINEARITIES IN UAV AUTOMATIC FLIGHT CONTROL SYSTEMS

Abstract

The linear or the nonlinear feature of systems being modelled or designed is a core property we should be familiar with before taking up any system design or analysis-related task. The dynamic model-based closed loop control design is widely used in control engineering when dynamic or static nonlinearities are considered to be present in the closed loop control system. This paper addresses both dynamical and static nonlinearities modelled and handled in the closed loop control system