Fixed wings UAV direction control “Hardware Design”

Khalil Abdallah, Mohamed and Hassan Abdalla Hashim, Aisha and Gasmalla, Tahani AbdallahAttia and Babiker, Sharief (2015) Fixed wings UAV direction control “Hardware Design”. International Journal of Computer Science and Network Security (IJCSNS), 15 (1). pp. 19-26. ISSN 1738-7906

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Abstract

The goal is to design of Unmanned Aerial Vehicle "UAV" system through the control of a stable fixed-wing aircraft to accomplish inexpensive, simple, and still efficient aircrafts by adding an inertial circuitry to the airplane that consists of a GPS unit, a microcontroller unit, and other devices. The aircraft has the ability to navigate from one place to another predefined place. Additional feature is to switch between two the modes of control: autopilot and manual is provided. In autopilot mode the aircraft is fully controlled by an on-board microcontroller, the only data needed for navigation is to specify the target waypoint, and then the system will navigate fully automatic towards the target until it reaches the target and does the specified duty.

Item Type:	Article (Journal)
Additional Information:	2523/41962
Uncontrolled Keywords:	UAV, Servo motor, GPS
Subjects:	T Technology > T Technology (General) > T10.5 Communication of technical information
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button):	Kulliyyah of Engineering > Department of Electrical and Computer Engineering
Depositing User:	Prof. Dr. Aisha Hassan Abdalla Hashim
Date Deposited:	06 Mar 2015 12:06
Last Modified:	16 Jun 2017 10:32
URI:	http://irep.iium.edu.my/id/eprint/41962

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