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| 題 名 | Eigenstructure Assignment of Control System Design Based on LEQG/LTR Method=利用線性指數二次高斯及迴路轉移回歸法從事控制系統特徵結構指定研究 |
|---|---|
| 作 者 | 張哲旭; 林君明; 蔡渙良; | 書刊名 | 中正嶺學報 |
| 卷 期 | 25:1 1996.07[民85.07] |
| 頁 次 | 頁99-114 |
| 分類號 | 448.942 |
| 關鍵詞 | 特徵結構指定; 線性指數二次高斯法; 迴路轉移回歸法; Eigenstructure assignment; Linear exponential quadratic gaussian; Loop transfer recovery; |
| 語 文 | 英文(English) |
| 中文摘要 | 本文提出一種以線性指數二次高斯及迴路轉移回歸法從事控制系統特徵結構指定 之強健性設計。由於以本法所設計最佳狀態控制器同時考慮系統本身及量測所產生的雜訊, 因此本文所提出的方法比線性二次高斯法更具強健性。本文推導一種同時考慮時域、頻域設 計規格及解交連設計法則,並以無人駕駛飛行器之實際模組來進行設計模擬,以說明本方法 對系統擾動、感測器雜訊及氣動力交互藕連更具強健性,同時時域響應亦較佳。 |
| 英文摘要 | The purpose of this paper is to develop a method for the Multi-Input Multi-Output (MMO) Eigenstructure Assignment (ESA) of control system design based on the Linear Exponential Quadratic Gaussian and Loop Transfer Recovery (LEQG/LTR) methodology. Since the control system obtained by the proposed method can take the covariances of both system and measurement noises into consideration, whereas the traditional LQG/LTR one cannot, the proposed method is more robust. This paper also derives the algorithms which can take all the time domain, frequency domain, and decoupling design techniques into a unified method. An example for lateral attitude control system design of an unmanned aircraft is given, which shows that the proposed method is more robust to distrubance, sensor noise, and aerodynamic cross-coupling, as well as better in the time-domain responses. |
本系統中英文摘要資訊取自各篇刊載內容。