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...
Main Authors: | Khalil Abdallah, Mohamed, Hassan Abdalla Hashim, Aisha, Gasmalla, Tahani AbdallahAttia, Babiker, Sharief |
---|---|
Format: | Article |
Language: | English |
Published: |
IJCSNS
2015
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/41962/ http://irep.iium.edu.my/41962/ http://irep.iium.edu.my/41962/1/20150103.pdf |
Similar Items
-
Implementation of direction control algorithms for fixed wings UAV
by: Abdalla, Mohamed K., et al.
Published: (2015) -
Development of communication module for semi-autonomos UAV and robots
by: Abdul Aziz, Normaziah, et al.
Published: (2012) -
Improving message delay, handoff latency and binding update in high level nested network mobility
by: Babiker, Mohammed Ali, et al.
Published: (2015) -
Evaluation of an enhanced scheme for high-level nested network mobility
by: Ali Mohammed, Mohammed Babiker, et al.
Published: (2015) -
Factors effecting fixed-line telecom services customer retention: A study of Pakistan
by: Rind, M. Malook, et al.
Published: (2016)