02207nam a2200265 a 4500 vtls000045972 KUKTEM 20251114204409.0 100603t2009 my dao f m 000 0 eng d THE0007774(Local) 201905241518 fawwaz 201107132213 VLOAD 201006041121 Fida 201006031630 Fida UMP UG1242 .D7 Z35 2009 rs Bc. Mohamed Zaid Mohamed Zakaria Weight distribution, stability and structural analysis for reconnaissance UAV / Mohamed Zaid Bin Mohamed Zakaria Weight distribution, stability and structural analysis for reconnaissance UAV [electronic resource] 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. Drone aircraft Stability of airplanes 0 0 0 1 20000 20000 2019-09-04 0 UG1242 .D7 Z35 2009 rs Bc. 0000046301 2019-09-04 00:00:00 1 2019-09-04 PSM 0 0 0 1 20000 20000 2019-09-04 0 CD 4451 | UG1242 .D7 Z35 2009 rs Bc. 0000046302 2019-09-04 00:00:00 1 2019-09-04 PSM VIRTUA40 1329 1335 VTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992