MARC details
| 000 -LEADER |
|---|
| fixed length control field |
02207nam a2200265 a 4500 |
| 001 - CONTROL NUMBER |
|---|
| control field |
vtls000045972 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
KUKTEM |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20251114204409.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
100603t2009 my dao f m 000 0 eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER |
|---|
| International Standard Book Number |
THE0007774(Local) |
| 039 #9 - LEVEL OF BIBLIOGRAPHIC CONTROL AND CODING DETAIL [OBSOLETE] |
|---|
| Level of rules in bibliographic description |
201905241518 |
| Level of effort used to assign nonsubject heading access points |
fawwaz |
| Level of effort used to assign subject headings |
201107132213 |
| Level of effort used to assign classification |
VLOAD |
| Level of effort used to assign subject headings |
201006041121 |
| Level of effort used to assign classification |
Fida |
| -- |
201006031630 |
| -- |
Fida |
| 040 ## - CATALOGING SOURCE |
|---|
| Original cataloging agency |
UMP |
| 090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN) |
|---|
| Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) |
UG1242 .D7 Z35 2009 rs Bc. |
| 100 0# - MAIN ENTRY--PERSONAL NAME |
|---|
| Personal name |
Mohamed Zaid Mohamed Zakaria |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Weight distribution, stability and structural analysis for reconnaissance UAV / |
| Statement of responsibility, etc. |
Mohamed Zaid Bin Mohamed Zakaria |
| 246 3# - VARYING FORM OF TITLE |
|---|
| Title proper/short title |
Weight distribution, stability and structural analysis for reconnaissance UAV |
| Medium |
[electronic resource] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
Kuantan, Pahang : |
| Name of publisher, distributor, etc. |
UMP , |
| Date of publication, distribution, etc. |
2009 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
xv , 63 p. : |
| Other physical details |
ill. (some col.) ; |
| Dimensions |
30 cm. + |
| Accompanying material |
1 computer disc |
| 502 ## - DISSERTATION NOTE |
|---|
| Dissertation note |
Project paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2009 |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE |
|---|
| Bibliography, etc. note |
Bibliography : p. 53 |
| 520 3# - SUMMARY, ETC. |
|---|
| Summary, etc. |
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. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Drone aircraft |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical term or geographic name entry element |
Stability of airplanes |