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Attitude pointing enhancement for combined energy and attitude control system |
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| Authors: | Renuganth Varatharajoo Choo Tech Wooi Musa Mailah |
| Institution: | 1. Department of Mathematics and Computer Science, University of Larbi Tebessi, Tebessa, 12002, Algeria;2. Department of Mathematics, Faculty of Science, Al-Balqa Applied University, Salt 19117, Jordan;3. Nonlinear Analysis and Applied Mathematics (NAAM) Research Group, Department of Mathematics, Faculty of Science, King Abdulaziz University, Jeddah 21589, Saudi Arabia;4. Department of Mathematics, Quaid-I-Azam University, Islamabad 44000, Pakistan |
| Abstract: | This paper extends the previous works that appeared in Acta Astronautica. An approach that incorporates the Active Force Control (AFC) technique into a conventional Proportional-Derivative (PD) controller is proposed for a 50 kg small satellite. Numerical treatments are performed to validate the effectiveness of AFC. The attitude control capability of the combined energy and attitude control system (CEACS) is expected to improve. The result shows an important attitude pointing enhancement for the CEACS attitude control task. |
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