Mohamed, K., hassan, M., Abdel Wahab, A., mamdouh, M., El Dahshan, A., Soleit, E. (2017). Design and Implementation of Satellite (Cubesat) Attitude Control Sub Systems. test, 2(Second International Undergraduate Research Conference, IUGRC), 108-108. doi: 10.21608/iugrc.2017.90648
Karim Mohamed; Mahmoud hassan; Ahmed Atef Abdel Wahab; Mohamed mamdouh; Abdellah El Dahshan; Elsayed Soleit. "Design and Implementation of Satellite (Cubesat) Attitude Control Sub Systems". test, 2, Second International Undergraduate Research Conference, IUGRC, 2017, 108-108. doi: 10.21608/iugrc.2017.90648
Mohamed, K., hassan, M., Abdel Wahab, A., mamdouh, M., El Dahshan, A., Soleit, E. (2017). 'Design and Implementation of Satellite (Cubesat) Attitude Control Sub Systems', test, 2(Second International Undergraduate Research Conference, IUGRC), pp. 108-108. doi: 10.21608/iugrc.2017.90648
Mohamed, K., hassan, M., Abdel Wahab, A., mamdouh, M., El Dahshan, A., Soleit, E. Design and Implementation of Satellite (Cubesat) Attitude Control Sub Systems. test, 2017; 2(Second International Undergraduate Research Conference, IUGRC): 108-108. doi: 10.21608/iugrc.2017.90648

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, Pages 108-108    PDF (611.34 K)
Document Type: Original Article
DOI: 10.21608/iugrc.2017.90648
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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