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Orbit selection for optical and radar remote sensing satellite / (Record no. 76043)

MARC details
000 -LEADER
fixed length control field 02001cam a2200325 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 191221s2019 ua dhb f m 000 0 eng d
040 ## - CATALOGING SOURCE
Original cataloging agency EG-GiCUC
Language of cataloging eng
Transcribing agency EG-GiCUC
041 0# - LANGUAGE CODE
Language code of text/sound track or separate title eng
049 ## - LOCAL HOLDINGS (OCLC)
Holding library Deposite
097 ## - Thesis Degree
Thesis Level M.Sc
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Classification number Cai01.12.01.M.Sc.2019.Mo.O
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Mohamed Sayed Ahmed Elzanaty
245 10 - TITLE STATEMENT
Title Orbit selection for optical and radar remote sensing satellite /
Statement of responsibility, etc. Mohamed Sayed Ahmed Elzanaty ; Supervised Mervat Elsayd Awad , Elamira Hend Said Khattab , Mohammad Ahmad Fouad Ali Basha
246 15 - VARYING FORM OF TITLE
Title proper/short title الاختيار الامثل لمدارات الاقمار الصناعية الكهروبصرية والرادارية للاستشعار عن بعد
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Mohamed Sayed Ahmed Elzanaty ,
Date of publication, distribution, etc. 2019
300 ## - PHYSICAL DESCRIPTION
Extent 117 P. :
Other physical details charts , facsimiles ;
Dimensions 25cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Science - Department of Astronomy and Meteorology
520 ## - SUMMARY, ETC.
Summary, etc. This thesis aimed to determine and select the best choice of orbits for low earth orbit satellite.The orbit selection procedures are very essential and complex, concerning swap between a numbers of various parameters where the designer picks the best orbital parameters to meet the mission requirements. The orbit typically defines the space mission lifetime, cost, environment, communication links, coverage, availability of launch vehicle, and the payload performance. The numerical and mathematical models are expressed to compute the satellite{u2019}s orbit by MATLAB software under the gravitational second zonal harmonic effect
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Access times of satellite
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Ground track of satellite
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term illumination condition
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Elamira Hend Said Khattab ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mervat Elsayd Awad ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohammad Ahmad Fouad Ali Basha ,
Relator term
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Shimaa
Reviser Cataloger
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Dewey Decimal Classification
Koha item type Thesis
Holdings
Source of classification or shelving scheme Not for loan Home library Current library Date acquired Full call number Barcode Date last seen Koha item type Copy number
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة قاعة الرسائل الجامعية - الدور الاول 11.02.2024 Cai01.12.01.M.Sc.2019.Mo.O 01010110080455000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.12.01.M.Sc.2019.Mo.O 01020110080455000 22.09.2023 CD - Rom 80455.CD