Satellite attitude tracking control using Lyapunov control theory
This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tracking manoeuver. The attitude reference trajectory is generated to track a ground object on the rotating Earth and to keep the Sun vector perpendicular to the solar panel to maximize the solar power...
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| 主要な著者: | , , |
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| フォーマット: | 論文 |
| 言語: | English English |
| 出版事項: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
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| 主題: | |
| オンライン･アクセス: | http://irep.iium.edu.my/74025/7/74025%20Satellite%20attitude%20tracking%20control.pdf http://irep.iium.edu.my/74025/8/74025%20Satellite%20attitude%20tracking%20control%20SCOPUS.pdf http://irep.iium.edu.my/74025/ https://www.ijrte.org/wp-content/uploads/papers/v7i6s/F02490376S19.pdf |
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| 要約: | This paper explores attitude control algorithms using thrusters and momentum wheels for satellite tracking
manoeuver. The attitude reference trajectory is generated to track a ground object on the rotating Earth and to keep the Sun vector perpendicular to the solar panel to maximize the solar power. The dynamic model is derived based on Newton-Euler approach and Modified Rodrigues Parameters (MRPs) are used to represent attitude kinematics. The control algorithms are derived based on the Lyapunov stability control theory to ensure the asymptotic stability of the control law. MATLAB software package is used as a simulation environment to develop and test the performance of the proposed tracking control algorithms using a Graphical User Interface (GUI) tool that can be expanded for future development. |
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