dc.Location	2014 TA 169 S23
dc.Supervisor	Professor Robert Whalley
dc.contributor.author	Al-Saadi, Ziad Abdulla
dc.date.accessioned	2014-10-19T06:00:30Z
dc.date.available	2014-10-19T06:00:30Z
dc.date.issued	2014-03
dc.description	DISSERTATION WITH DISTINCTION
dc.description.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.	en_US
dc.identifier.other	100067
dc.identifier.uri	http://bspace.buid.ac.ae/handle/1234/690
dc.language.iso	en	en_US
dc.publisher	The British University in Dubai (BUiD)	en_US
dc.subject	multivariable feedback control	en_US
dc.subject	aircraft carrier landing	en_US
dc.title	A Design Study for a Multivariable Feedback Controller for Aircraft Carrier Landing	en_US
dc.type	Dissertation	en_US

A Design Study for a Multivariable Feedback Controller for Aircraft Carrier Landing