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Inverse simulation with feedback technique for aircraft motion along prescribed trajectories / (Record no. 18915)

MARC details
000 -LEADER
fixed length control field 015550000a22003250004500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223025716.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 081227s2008 ua d 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 Cai01.13.01.M.Sc.2008.Is.I
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Islam Salah Ahmed Elbahnasy
245 10 - TITLE STATEMENT
Title Inverse simulation with feedback technique for aircraft motion along prescribed trajectories /
Statement of responsibility, etc. Islam Salah Ahmed Elbahnasy ; Supervised Mohamed Madbouli Abdelrahman
246 15 - VARYING FORM OF TITLE
Title proper/short title المحاكاة العكسية بإستخدام التغذية الرجعية لحركة الطائرة على المسارات سابقة التحديد
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Islam Salah Ahmed Elbahnasy ,
Date of publication, distribution, etc. 2008
300 ## - PHYSICAL DESCRIPTION
Extent 107P. :
Other physical details charts ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis(M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. This study looks at the application of the inverse simulation in fight dynamics the aim of this study is to provide technique to be used onboard aircraft as control system the technique is developed based on the classical PD control algorithm the aircraft prescribed trajectory was modeled as polynomial function
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Aircraft
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Inverse
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Simulation
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohamed Madbouli Abdelrahman ,
Relator term
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://172.23.153.220/th.pdf">http://172.23.153.220/th.pdf</a>
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Enas
Reviser Cataloger
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Mustafa
Reviser Revisor
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 Cai01.13.01.M.Sc.2008.Is.I 01010110050297000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.M.Sc.2008.Is.I 01020110050297000 22.09.2023 CD - Rom 50297.CD