ICAR Research Data Repository for Knowledge Management
Design of Aircraft Control System
KrishiKosh
View Archive Info| Field | Value | |
| Title |
Design of Aircraft Control System
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| Creator |
Elmajdub, Naser. F.AB.
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| Contributor |
Srivastava, Manish Kumar
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| Subject |
null
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| Description |
Ph. d. thesis
The two important stages of aircraft – takeoff and landing are to be designed in this thesis. In physical form, it is very difficult to study the takeoff and landing stages of aircraft. In this thesis, the new way is included to analyses the takeoff and landing of aircraft by SIMULINK which is the branch of MATLAB. On MATLAB simulator, it can see the takeoff and landing position of aircraft and analysis the graphs on different parameters. The take-off and landing of an aircraft is often the most critical and accident prone portion. This thesis describes the design of an aircraft take-off and landing algorithm implemented on an existing low-cost flight control system with six degree of freedom (6-DoF). This thesis also describes the takeoff and landing algorithm development and gives validation results from MATLAB in the loop simulation. The scope of the thesis is reaches to the best situation to the design of aircraft control systems in most common high risk phases at important two stages with use SIMULINK program, high performance in short runway and how change the classical design used the control system from mechanical to hydro mechanical into electrical control system as used in modern aircraft with Fly-By-Wire but in the future design technology Fly-By-Light may be used. The takeoff and landing control system is designed under constraints as degree of freedom and the equation of motion to be improved in many situations. The research is achieved by MATLAB/Simulink. The simulation results show that the control system performs well. The proposed approach gets the information of attitude and altitude by using aircraft model and various indicators shows the actual reading in aircraft model. The three classes of models and simulations are virtual, constructive and live. |
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| Date |
2017-12-20T05:55:08Z
2017-12-20T05:55:08Z 2017 |
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| Type |
Thesis
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| Identifier |
http://krishikosh.egranth.ac.in/handle/1/5810037898
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| Language |
en
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| Format |
application/pdf
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| Publisher |
FACULTY OF ENGINEERING AND TECHNOLOGY SAM HIGGINBOTTOM UNIVERSITY OF AGRICULTURE, TECHNOLOGY AND SCIENCES Deemed-to-be-University (FORMERLY ALLAHABAD AGRICULTURAL INSTITUTE) NAINI, ALLAHABAD-211007
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