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Attitude estimation and control of a ducted fan VTOL UAV

dc.contributor.advisorTayebi, Abdelhamid
dc.contributor.authorRoberts, Andrew David
dc.date.accessioned2017-06-08T13:20:45Z
dc.date.available2017-06-08T13:20:45Z
dc.date.created2007
dc.date.issued2007
dc.identifier.urihttp://knowledgecommons.lakeheadu.ca/handle/2453/3699
dc.description.abstractA significant area of current research is to develop aircraft which are unmanned. More specifically, some researchers are focusing on hovering type aircraft, or vertical take-off and landing (VTOL) aircraft. Since these types of aircraft do not need to be constantly in motion to maintain lift, they have certain advantages over fixed-wing aircraft. Suitable applications could involve aerial photography, atmospheric measurements or surveillance and defense. The most common type of VTOL aircraft is the helicopter. One disadvantage of this aircraft is the degree of danger involved due to the exposed rotor blades. This is one motivating factor behind the 'ducted fan' system. This type of system uses a rotor which is enclosed in a aerodynamically shaped duct.
dc.language.isoen_US
dc.subjectVertically rising aircraft (Automatic control)
dc.subjectRotors (Automatic control)
dc.subjectDrone aircraft
dc.titleAttitude estimation and control of a ducted fan VTOL UAV
dc.typeThesis
etd.degree.nameMaster of Science
etd.degree.levelMaster
etd.degree.disciplineEngineering : Control
etd.degree.grantorLakehead University


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