Design and Implementation of Satellite (Cubesat) Attitude Control Sub Systems | ||||
The International Undergraduate Research Conference | ||||
Article 29, Volume 2, Second International Undergraduate Research Conference, IUGRC, 2017, Page 108-108 PDF (611.34 K) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/iugrc.2017.90648 | ||||
View on SCiNiTO | ||||
Authors | ||||
Karim Mohamed1; Mahmoud hassan1; Ahmed Atef Abdel Wahab1; Mohamed mamdouh1; Abdellah El Dahshan2; Elsayed Soleit2 | ||||
1High Institute For Engineering and Technology Al Obour, cairo,Egypt. | ||||
2Prof.Dr, High Institute For Engineering and Technology Al Obour, cairo,Egypt. | ||||
Abstract | ||||
The Objective of this graduation project is to design and develop of a powerful attitude control sub Systems that may be used in the next Egyptian CubeSat mission. The trend now is to use reaction wheels (RW) actuators in CubeSat missions. RW operate by accelerating a wheel in one direction and thereby forcing the satellite to rotate in the other direction. One widely used actuation system is Reaction Wheels (RW) which mainly has been used for larger satellites. The students are involved to build up a powerful attitude control sub System practically. The implemented module is successfully tested and its performance is measured via computer simulation (MATlab) and real time implementation using the optimal controller ARDUINO type MEGA2560. The results are encouraged. | ||||
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