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