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Design and implementation of the para-real flight system for aircrafts and autopilots ground testing / (Record no. 60199)

MARC details
000 -LEADER
fixed length control field 02957cam a2200349 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223031701.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 170311s2016 ua o 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 Ph.D
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Classification number Cai01.13.01.Ph.D.2016.Os.D
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Osama Saaid Mohamady Abdelrazek
245 10 - TITLE STATEMENT
Title Design and implementation of the para-real flight system for aircrafts and autopilots ground testing /
Statement of responsibility, etc. Osama Saaid Mohamady Abdelrazekc ; Supervised Sayed Desouki Hassan , Gamal Mahmoud Sayed Elbayoumi , Basman Eelhadidi
246 15 - VARYING FORM OF TITLE
Title proper/short title تصميم و تنفيذ نظام طيران شبه حقيقى لاختبار الطائرات و الطيار الآلى
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Osama Saaid Mohamady Abdelrazek ,
Date of publication, distribution, etc. 2016
300 ## - PHYSICAL DESCRIPTION
Extent 157 P. :
Other physical details photographs ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. The objective of this thesis is to design and implement the para-real flight system. The system is designed for ground testing of aircrafts, its subsystems, and autopilots. The para-real flight system is implemented in a wind tunnel that can test aircraft models up to 0.55 m wing span under controlled wind speed up to 20 m/s. A test rig is designed to hold the model and control the flow angle of attack and side slip angle. The rig is designed to deliver power to the model in the tunnel and to fully actuate the model. The forces and moments acting on the model are measured by six components force and torque sensor. A three dimensional flight simulator is developed to demonstrate the movement of the model undergoing test in the tunnel. The simulator uses instantaneous measurements of forces and moments to determine flight conditions. A static test is performed to assess the methodology of measuring the forces and moments acting on the tested model. The measurements are compared to a numerically computed data for a mini UAV model in various flight conditions. Several tests are conducted to get the para-real flight system limitations and calibration. A conventional mini UAV and unconventional mini flying wing UAV are equipped with data gathering system to acquire its real flight data. 45% and 40% scaled models are prepared to be tested by the para-real flight system. The experimental results show that the present para-real flight system has limited capabilities but the para-real flight system idea is applicable and promising
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Aircraft testing
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Para-real flight
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Unmanned aerial vehicles
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Basman Elhadidi ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Gamal Mahmoud Sayed Elbayoumi ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Sayed Desouki Hassan ,
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 Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Samia
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 Cai01.13.01.Ph.D.2016.Os.D 01010110071265000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.Ph.D.2016.Os.D 01020110071265000 22.09.2023 CD - Rom 71265.CD