Fixed wings UAV direction control “Hardware Design”
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...
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iium-419622017-06-16T02:32:04Z http://irep.iium.edu.my/41962/ Fixed wings UAV direction control “Hardware Design” Khalil Abdallah, Mohamed Hassan Abdalla Hashim, Aisha Gasmalla, Tahani AbdallahAttia Babiker, Sharief T10.5 Communication of technical information 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. IJCSNS 2015-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/41962/1/20150103.pdf 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 http://ijcsns.org/ |
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Local University |
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International Islamic University Malaysia |
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IIUM Repository |
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Online Access |
language |
English |
topic |
T10.5 Communication of technical information |
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T10.5 Communication of technical information Khalil Abdallah, Mohamed Hassan Abdalla Hashim, Aisha Gasmalla, Tahani AbdallahAttia Babiker, Sharief Fixed wings UAV direction control “Hardware Design” |
description |
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. |
format |
Article |
author |
Khalil Abdallah, Mohamed Hassan Abdalla Hashim, Aisha Gasmalla, Tahani AbdallahAttia Babiker, Sharief |
author_facet |
Khalil Abdallah, Mohamed Hassan Abdalla Hashim, Aisha Gasmalla, Tahani AbdallahAttia Babiker, Sharief |
author_sort |
Khalil Abdallah, Mohamed |
title |
Fixed wings UAV direction control “Hardware Design” |
title_short |
Fixed wings UAV direction control “Hardware Design” |
title_full |
Fixed wings UAV direction control “Hardware Design” |
title_fullStr |
Fixed wings UAV direction control “Hardware Design” |
title_full_unstemmed |
Fixed wings UAV direction control “Hardware Design” |
title_sort |
fixed wings uav direction control “hardware design” |
publisher |
IJCSNS |
publishDate |
2015 |
url |
http://irep.iium.edu.my/41962/ http://irep.iium.edu.my/41962/ http://irep.iium.edu.my/41962/1/20150103.pdf |
first_indexed |
2023-09-18T20:59:55Z |
last_indexed |
2023-09-18T20:59:55Z |
_version_ |
1777410554377273344 |