MODELLING AND LQR BASED LINEARIZED CONTROL STRATEGY OF QUAD ROTOR AIRCRAFT

dc.contributor.author	Akhtar, Tehseen
dc.date.accessioned	2023-08-18T11:05:10Z
dc.date.available	2023-08-18T11:05:10Z
dc.date.issued	2012
dc.identifier.other	2010-NUST-MS PhD-MTS-25
dc.identifier.uri	http://10.250.8.41:8080/xmlui/handle/123456789/36905
dc.description	Supervisor: Dr. Knuwar Faraz	en_US
dc.description.abstract	In this paper, a non-linear modal of quad-rotor aircraft is derived (which is an underactuated with six degrees of freedom (6DOF) is derived) using the basic laws of physics. The derived model is highly unstable, so first the model is linearized and then a linear multivariable control strategy is developed for the purpose of first stabilizing the aircraft and secondly forcing the aircraft to follow a certain fix reference value. The performance of this linear control strategy is evaluated using simulations on Simulink/MATLAB and the results show the effectiveness of the LQR controllers.	en_US
dc.language.iso	en	en_US
dc.publisher	College of Electrical & Mechanical Engineering (CEME), NUST	en_US
dc.title	MODELLING AND LQR BASED LINEARIZED CONTROL STRATEGY OF QUAD ROTOR AIRCRAFT	en_US
dc.type	Thesis	en_US