Please use this identifier to cite or link to this item: https://bspace.buid.ac.ae1234/690
Title: A Design Study for a Multivariable Feedback Controller for Aircraft Carrier Landing
Authors: Al-Saadi, Ziad Abdulla
Keywords: multivariable feedback control
aircraft carrier landing
Issue Date: Mar-2014
Publisher: The British University in Dubai (BUiD)
Abstract: This research studies the design of a multivariable control system for aircraft landing. To improve the safety of aircraft landing, handling quality is improved whilst decreasing the number of critical tasks the pilot has to perform simultaneously with improved responsiveness of the aircraft to the pilot’s input commands. By adding another control surface on aircraft’s horizontal tail the dynamics of the aircraft motion are improved, and the pilot has the minimum number of inputs to effectively control the aircraft. Simulation of the results demonstrate the effectiveness of the dynamic reaction and steady state system response showing the aircraft response to tailplane or aileron input change. Least effort controller design method provides superior results motivating further application studies.
Description: DISSERTATION WITH DISTINCTION
URI: http://bspace.buid.ac.ae/handle/1234/690
Appears in Collections:Dissertations for Systems Engineering (SE)

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