Estimation And Analysis Of Performance, Stability And Control For Unmanned Aerial Vehicle (Uav) Tamingsari Using Semiempirical Method

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dc.contributor.authorMohd Arshad, Aizam Shahroni
dc.date.accessioned2018-09-19T03:13:50Z
dc.date.available2018-09-19T03:13:50Z
dc.date.issued2010-09
dc.description.abstractThis thesis gives deep insight on the estimation and analysis of flight performance, stability and control derivatives particularly for unmanned aerial vehicle (UAV), based on semiempirical methods. UAV is airplane that have no human onboard, but rather are flown autonomously or piloted remotely. It is commonly used in many countries to develop tasks such as surveillance, research or combat due to its autonomy of flight. UAV Tamingsari was selected to be a research case, which belong to the School of Aerospace Engineering, Universiti Sains Malaysia. The results obtained from semiempirical methods have been validated by Advance Aircraft Analysis (AAA) computational software as a tool to check the validity. The validation results of UAV Tamingsari have shown good agreement for most of the parameters analyzed. In this manner, the results showed that the semiempirical methods provide good prediction of aerodynamics, flight performance, stability and control derivatives for UAV Tamingsari due to its approximate geometry inputs, which used to evaluate the UAV configuration.This thesis gives deep insight on the estimation and analysis of flight performance, stability and control derivatives particularly for unmanned aerial vehicle (UAV), based on semiempirical methods. UAV is airplane that have no human onboard, but rather are flown autonomously or piloted remotely. It is commonly used in many countries to develop tasks such as surveillance, research or combat due to its autonomy of flight. UAV Tamingsari was selected to be a research case, which belong to the School of Aerospace Engineering, Universiti Sains Malaysia. The results obtained from semiempirical methods have been validated by Advance Aircraft Analysis (AAA) computational software as a tool to check the validity. The validation results of UAV Tamingsari have shown good agreement for most of the parameters analyzed. In this manner, the results showed that the semiempirical methods provide good prediction of aerodynamics, flight performance, stability and control derivatives for UAV Tamingsari due to its approximate geometry inputs, which used to evaluate the UAV configuration.en_US
dc.identifier.urihttp://hdl.handle.net/123456789/6592
dc.language.isoenen_US
dc.publisherUniversiti Sains Malaysiaen_US
dc.subjectUnmanned Aerial Vehicle (Uav)en_US
dc.subjectTamingsari Using Semiempirical Methoden_US
dc.titleEstimation And Analysis Of Performance, Stability And Control For Unmanned Aerial Vehicle (Uav) Tamingsari Using Semiempirical Methoden_US
dc.typeThesisen_US
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