Academic Journal
Attitude stabilization of spacecraft simulator based on modified constrained feedback linearization model predictive control
| العنوان: | Attitude stabilization of spacecraft simulator based on modified constrained feedback linearization model predictive control |
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| المؤلفون: | Maria Khodaverdian, Maryam Malekzadeh |
| المصدر: | IET Control Theory & Applications, Vol 17, Iss 8, Pp 953-967 (2023) |
| بيانات النشر: | Wiley, 2023. |
| سنة النشر: | 2023 |
| مصطلحات موضوعية: | attitude control, constraint satisfaction problems, predictive control, Control engineering systems. Automatic machinery (General), TJ212-225 |
| الوصف: | Abstract This paper aims to discuss the approach of constrained modified feedback linearization model predictive control for the spacecraft simulator. By utilizing the high accuracy and constrained properties of model predictive control (MPC), an optimum MPC is designed for the spacecraft feedback linearized system. The composite controller has the ability to control both the attitude and angular velocity of the reaction wheels (i.e. steering the angular momentum to zero at the end of the maneuver). The simulation and experimental results demonstrate that the proposed hybrid controller has an insignificant calculative cost and facilitates the spacecraft to perform regulation maneuver with sufficient precision in the presence of external torques and actuator saturations. |
| نوع الوثيقة: | article |
| وصف الملف: | electronic resource |
| اللغة: | English |
| تدمد: | 1751-8652 1751-8644 |
| Relation: | https://doaj.org/toc/1751-8644; https://doaj.org/toc/1751-8652 |
| DOI: | 10.1049/cth2.12429 |
| URL الوصول: | https://doaj.org/article/2108407d90c04939a2f81c2cf9d51422 |
| رقم الانضمام: | edsdoj.2108407d90c04939a2f81c2cf9d51422 |
| قاعدة البيانات: | Directory of Open Access Journals |
Full Text Finder | تدمد: | 17518652 17518644 |
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| DOI: | 10.1049/cth2.12429 |