Automat Control of the Aircrafts- Lateral Movement using the Dynamic Inversion

The paper presents a new system for the automat control of the aircrafts’ flight in lateral plane using the cinematic model and the dynamic inversion. Starting from the equations of the aircrafts’ lateral movement, the authors use two axes systems and obtained a control law that cancels the lateral deviation of the flying objects from the runway line. This system makes the aircrafts’ direction angle to follow the direction angle of the runway line. Simulations in Matlab/Simulink have been done for different aircraft’s initial points and direction angles. The inconvenience of this system is the long duration of the “transient regime”. That is why this system can be used independently, but the results are not very good; thus, it can be a part (subsystem) of other systems. The main system that cancels the lateral deviation from the runway line is based on dynamic inversion and uses, as subsystem, the control system for the lateral movement using the cinematic model. Using complex Matlab/Simulink models, the authors obtained the time evolution of the direction angle and the time evolution of the aircraft lateral deviation with respect to the runway line, for different values of the initial direction angle and for different wind types. The system has a very good behavior for all initial direction angles and wind types. Keywords—Direction angle, Dynamic inversion, Lateral deviation, Lateral movement