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Weight distribution, stability and structural analysis for reconnaissance UAV / Mohamed Zaid Bin Mohamed Zakaria

By:

Mohamed Zaid Mohamed Zakaria

Material type: Text

TextPublication details: Kuantan, Pahang : UMP , 2009Description: xv , 63 p. : ill. (some col.) ; 30 cm. + 1 computer discISBN:

THE0007774(Local)

Other title:

Weight distribution, stability and structural analysis for reconnaissance UAV [electronic resource]

Subject(s):

Dissertation note: Project paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2009 Abstract: UAV is a new pattern of surveillances system that has being used in for many purposes this day. However, smaller UAVs are needed for friendlier handling. This is a Mini UAV which capable to compete with other Mini UAV in the market now days. In this project, the focus is to analyze and design the airframe of the Mini UAV. The UAV is 2m in span and 1.2m in length and takeoff weight of 3.8 kg. it is light weight, so the stability on the highest altitude has to be considered as very important. The estimation of location of wing on the fuselage and its relevancy of the wingspan has to converge with the wing area. The weight plays an important specification for the UAV. The entire component including the power plant has to light. The placements of weight in the fuselage can change the position of center of gravity. The function of the UAV would affect the placement of component in the fuselage. The more stable the UAV the more reliable it'll be. The method of iteration is going to be used for calculation and analysis for. The CAD model will be designed using SolidWork.

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Holdings ( 2 )
Title notes ( 3 )

Holdings
Item type	Current library	Call number	Copy number	Status	Date due	Barcode
Final Year Report	UMPLIB PEKAN	UG1242 .D7 Z35 2009 rs Bc. (Browse shelf(Opens below))	1	Not for loan		0000046301
Final Year Report	UMPLIB PEKAN	CD 4451 \| UG1242 .D7 Z35 2009 rs Bc. (Browse shelf(Opens below))	1	Not for loan		0000046302

Project paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2009

Bibliography : p. 53

UAV is a new pattern of surveillances system that has being used in for many purposes this day. However, smaller UAVs are needed for friendlier handling. This is a Mini UAV which capable to compete with other Mini UAV in the market now days. In this project, the focus is to analyze and design the airframe of the Mini UAV. The UAV is 2m in span and 1.2m in length and takeoff weight of 3.8 kg. it is light weight, so the stability on the highest altitude has to be considered as very important. The estimation of location of wing on the fuselage and its relevancy of the wingspan has to converge with the wing area. The weight plays an important specification for the UAV. The entire component including the power plant has to light. The placements of weight in the fuselage can change the position of center of gravity. The function of the UAV would affect the placement of component in the fuselage. The more stable the UAV the more reliable it'll be. The method of iteration is going to be used for calculation and analysis for. The CAD model will be designed using SolidWork.