%0 Journal Article
%T DISCRETE-TIME VARIABLE STRUCTURE CONTROLLER FOR AIRCRAFT FLIGHT ANGLE TRACKING
%A Iskrenovic-Momcilovic
%A Olivera
%J -
%D 2014
%X Sa£żetak The paper presents the longitudinal, short-period aircraft dynamics and its application on the climb angle tracking. For the aircraft flight angle tracking the stable system centre technique is developed for controlling the output in a discrete-time non-minimum phase causal system using the sliding mode control. The developed discrete-time stable system centre technique transforms the output tracking problem to a corresponding state variable tracking problem by asymptotically identifying the ideal internal dynamics for the unstable internal states of a discrete-time system. A numerical simulation example is given to show the effectiveness of the method
%K discrete-time non-minimum phase system
%K stable system centre
%K sliding mode control
%U https://hrcak.srce.hr/index.php?show=clanak&id_clanak_jezik=191519