High-precision controller using LMI method for three-axis flexible satellite attitude stabilisation
Autor: | B.J. Eddine, K. Boulanouar, B. Elhassen |
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Rok vydání: | 2023 |
Předmět: | |
Zdroj: | The Aeronautical Journal. :1-12 |
ISSN: | 2059-6464 0001-9240 |
Popis: | This paper considers the problem of a three-axis flexible satellite attitude stabilisation subject to the vibration of flexible appendages and external environmental disturbances, which affect the rigid body motion. To solve this problem, a disturbance observer is proposed to estimate and thereby reject the flexible appendage vibration. Based on the H∞ and Linear Matrix Inequality (LMI) approach, a controller for spacecraft with flexible appendages is proposed to ensure robustness as well as attitude stability with high precision. Stability analysis of the overall closed-loop system is provided via the Lyapunov method. The simulation results of three-axis flexible spacecraft demonstrate the robustness and effectiveness of the proposed method. |
Databáze: | OpenAIRE |
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