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Helicopter modeling, trim and inverse simulation / (Record no. 61050)

MARC details
000 -LEADER
fixed length control field 02665cam a2200325 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223031727.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 170603s2016 ua 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.2016.Ha.H
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Hassan Shahat Hassan Abdelraof
245 10 - TITLE STATEMENT
Title Helicopter modeling, trim and inverse simulation /
Statement of responsibility, etc. Hassan Shahat Hassan Abdelraof ; Supervised Mohamed Madbouly Abdelrahman
246 15 - VARYING FORM OF TITLE
Title proper/short title الاتزان الديناميكى و المحاكاه العكسية لطائرة هليكوبتر
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Hassan Shahat Hassan Abdelraof ,
Date of publication, distribution, etc. 2016
300 ## - PHYSICAL DESCRIPTION
Extent 120 P. ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. The complex configuration of helicopter guarantee that the vehicle modeling, trim and simulation is significantly more difficult than fixed wing aircrafts. In this thesis, general expressions for the aerodynamic force and moment components acting on helicopter due to both main and tail rotors are driven by using the momentum theory and the blade element theory. These expressions are used in the rigid body equations of motion to build a general nonlinear model for single main rotor and tail rotor helicopter. This general model is used to get the helicopter response due to any set of control inputs, this process is denoted as direct simulation. Also, It can be used in control system design, studying the helicopter stability characteristics, and investigation of the vehicle handing qualities. The trim problem is solved at several flight conditions; any flight path angle, side slip angle and spinning rate. The inverse simulation; the process of obtaining the control inputs required by the pilot to achieve any maneuver, is solved by the differentiation approach. This approach is based on converting the differential equations to nonlinear algebraic equations which can be solved at each time step. The accuracy of this technique is improved by increasing the order of the differentiation scheme and decreasing the time step. The verification of the trim and inverse simulation results is achieved by supplying the resultant control inputs to the direct simulation code and the helicopter fly in the desired track
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Helicopter
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Modeling
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Trim
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohamed Madbouly 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 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.M.Sc.2016.Ha.H 01010110071766000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.M.Sc.2016.Ha.H 01020110071766000 22.09.2023 CD - Rom 71766.CD