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頁籤選單縮合
題名 | 微衛星強健性姿態容錯控制=Micro-Satellite Robust Attitude Fault Tolerant Control |
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作者 | 壽鶴年; 劉怡妠; 柳復華; 林麗鳳; | 書刊名 | 航空技術學院學報 |
卷期 | 10:1 2011.08[民100.08] |
頁次 | 頁103-114 |
分類號 | 448.942 |
關鍵詞 | 強健姿態控制; 輸出回授控制器; 線性矩陣不等式; Robust fault-tolerant H∞ control; Output-feedback controller; Linear matrix inequality; |
語文 | 中文(Chinese) |
中文摘要 | 本文探討微衛星強建姿態控制問題,當微衛星致動器和感測器失效情況下同時考慮系統中的不確定性的強建容錯H∞控制,運用線性矩陣不等式方法,採用所設計的輸出回授控制器,提出一種當任意致動器機構和感測器出現故障時,閉迴路系統仍保持漸近穩定且滿足給定的干擾衰減性能指標輸出迴授。將強健容錯控制設計方法應用於微衛星姿態控制系統的容錯控制並進行了模擬,模擬結果驗證了方法的有效性。 |
英文摘要 | The robust fault-tolerant H∞ control problem of uncertain linear system is studied in this paper.The solution of this problem is obtained for a H∞ output-feedback controller by a linear matrix inequality(LMI) approach.The simulation of a satellite attitude control system with actuator and sensor faults validates that this solution is effective. |
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