Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/23020
Full metadata record
DC FieldValueLanguage
dc.contributor.authorHerdawatie, Abdul Kadir-
dc.contributor.authorMohd. Rizal, Arshad, Engr. Assoc. Prof. Dr.-
dc.date.accessioned2013-01-17T08:38:40Z-
dc.date.available2013-01-17T08:38:40Z-
dc.date.issued2012-06-
dc.identifier.citationThe Journal of the Institution of Engineers, Malaysia, vol. 73(2), 2012, pages 26-33en_US
dc.identifier.issn0126-513X-
dc.identifier.urihttp://www.myiem.org.my/content/iem_journal_2012-361.aspx-
dc.identifier.urihttp://dspace.unimap.edu.my/123456789/23020-
dc.descriptionLink to publisher's homepage at http://www.myiem.org.my/en_US
dc.description.abstractAerial perspective provide great viewing window especially for surveillance and exploration activities. In responding to the need of green technology, airship is the best alternative for environmental friendly technology. In addition, airship is safer for low altitudes flying and able to maneuver at low speed in confined area. In order to drive the airship to the desired position, the airship’s rudder must generate a yaw angle. Therefore, this paper presents the techniques to control the navigation path of an airship through the yawing state response. To provide good airship heading, optimal control and feedback control technique were proposed. The main goal is to produce an appropriate output signal by controlling the rudder deflection while reducing the excessive movements of the vehicles. The simulation demonstrate that the proposed controller effectively reduced the excessive movement for yaw rate and roll angle of the airship. It is shown that closed loop system has an error less than 1.6% with minimum overshoot of 2.04%. Comparatively, better results were obtained by introducing higher gain to the optimal controller thus contribute to low control response.en_US
dc.language.isoenen_US
dc.publisherThe Institution of Engineers, Malaysia (IEM)en_US
dc.subjectAirshipen_US
dc.subjectLighter than air (LTA)en_US
dc.subjectLinear Quadratic Regulator (LQR)en_US
dc.subjectOptimal controlen_US
dc.subjectState feedbacken_US
dc.titleModelling and control of airship for low altitude surveillances applicationen_US
dc.typeArticleen_US
dc.contributor.urlwatie@uthm.edu.myen_US
dc.contributor.urlrizal@eng.usm.myen_US
Appears in Collections:IEM Journal

Files in This Item:
File Description SizeFormat 
ModelLing and Control of Airship for Low Altitude Surveillances Application.pdf429.65 kBAdobe PDFView/Open


Items in UniMAP Library Digital Repository are protected by copyright, with all rights reserved, unless otherwise indicated.