UAV Pitch Control System Analysis and Design

zomrawi, Ahmed Mohammed; Mohammed, Mazin saif aldeen Yosef; jedo, Mashaer Ibrahim Mustafa; Supervisor-, Ishraga Adzharia

dc.contributor.author	zomrawi, Ahmed Mohammed
dc.contributor.author	Mohammed, Mazin saif aldeen Yosef
dc.contributor.author	jedo, Mashaer Ibrahim Mustafa
dc.contributor.author	Supervisor-, Ishraga Adzharia
dc.date.accessioned	2018-01-21T13:33:12Z
dc.date.available	2018-01-21T13:33:12Z
dc.date.issued	2017-10-01
dc.identifier.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.	en_US
dc.identifier.uri	http://repository.sustech.edu/handle/123456789/20110
dc.description	Bachelors search	en_US
dc.description.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.	en_US
dc.description.sponsorship	Sudan University of Science and Technology	en_US
dc.language.iso	en	en_US
dc.publisher	Sudan University of Science and Technology	en_US
dc.subject	UAV Pitch	en_US
dc.subject	System Analysis and Design	en_US
dc.title	UAV Pitch Control System Analysis and Design	en_US
dc.type	Thesis	en_US