Weight distribution, stability and structural analysis for reconnaissance UAV /
Mohamed Zaid Mohamed Zakaria
Weight distribution, stability and structural analysis for reconnaissance UAV / Weight distribution, stability and structural analysis for reconnaissance UAV [electronic resource] Mohamed Zaid Bin Mohamed Zakaria - Kuantan, Pahang : UMP , 2009 - xv , 63 p. : ill. (some col.) ; 30 cm. + 1 computer disc
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.
THE0007774(Local)
Drone aircraft
Stability of airplanes
Weight distribution, stability and structural analysis for reconnaissance UAV / Weight distribution, stability and structural analysis for reconnaissance UAV [electronic resource] Mohamed Zaid Bin Mohamed Zakaria - Kuantan, Pahang : UMP , 2009 - xv , 63 p. : ill. (some col.) ; 30 cm. + 1 computer disc
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.
THE0007774(Local)
Drone aircraft
Stability of airplanes