Please use this identifier to cite or link to this item: https://repository.sustech.edu/handle/123456789/20110
Title: UAV Pitch Control System Analysis and Design
Authors: zomrawi, Ahmed Mohammed
Mohammed, Mazin saif aldeen Yosef
jedo, Mashaer Ibrahim Mustafa
Supervisor-, Ishraga Adzharia
Keywords: UAV Pitch
System Analysis and Design
Issue Date: 1-Oct-2017
Publisher: Sudan University of Science and Technology
Citation: zomrawi, Ahmed Mohammed.UAV Pitch Control System Analysis and Design/Ahmed Mohammed zomrawi,Mazin saif aldeen Yosef Mohammed,Mashaer Ibrahim Mustafa jedo;Ishraga Adzharia.-Khartoum : Sudan University of Science and Technology, College of Engineering,2017.-51 p. :ill;28cm.- Bachelors search.
Abstract: The ability of UAV to do a certain task is mainly dependent on accuracy of its control system. The purpose of this project is to analyze and design pitch control system for the UAV model in short mode, Too long settling time is noted after the model whose aerodynamic data are available have been analyzed by Using Simulink. The main objective of this research is to Suggest and design one of the suitable controllers to Control the model. The result obtained when applying PID controller is not satisfactory. Good result is obtained by using state feedback controller to control pitch. And the system has been stable upon the step input.
Description: Bachelors search
URI: http://repository.sustech.edu/handle/123456789/20110
Appears in Collections:Bachelor of Engineering

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