Switching Control Strategies for Aircraft Lateral Dynamics

Abstract

Due to the rapid growth of aircraft systems in the space, the implementation of a more optimized controller for aircraft dynamics control while the system is corrupted by sounds is quite a competitive position at the moment. When transitioning from one mode to other causes significant flight-critical differences in the aircraft dynamics, multi-mode switching between controllers corresponding to distinct modes of operation is required from the perspective of flight control design. It was demonstrated that a wide range of switching control techniques may be generated logically from the fundamental framework, proving the applicability of the suggested strategy. Using the MATLAB/SIMULINK platform, the switching control techniques presented in this research are tested for the longitudinal dynamics of aircraft systems.