Volosheniuk D. Information technology for controlling aircraft landings along virtual curvilinear trajectories

The thesis proposes an information technology for controlling the landing of aircraft by virtual curvilinear trajectory, which is based on the theories of terminal and intelligent control, the theory of nonlinear invariance. The main purpose is to increase the efficiency, environmental friendliness and safety at the landing stage of flights. Methods, algorithms and a system have been developed that predict the state and dynamics of an aircraft flight, and also take into account the distributed control environment, differences in accordance with the norms of safe separation, and minimization of the occurrence of conflict situations. The thesis solves an important scientific and applied problem of improving methods and models and the development of information technology for controlling an aircraft during an approach, to support decision-making in constructing an optimal landing trajectory and improving the safety of aircraft flights, as well as economic and environmental indicators of the use of aviation technology.