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DISCRETE-TIME VARIABLE STRUCTURE CONTROLLER FOR AIRCRAFT FLIGHT ANGLE TRACKING

Olivera Iskrenovic-Momcilovic orcid.org/0000-0003-0162-4416 ; Faculty of Education, University of Novi Sad, Serbia

Sažetak

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.

Ključne riječi

discrete-time non-minimum phase system; stable system centre; sliding mode control

Hrčak ID:

129616

URI

https://hrcak.srce.hr/129616

Datum izdavanja:

19.11.2014.

Posjeta: 1.213 *