| 研究生: |
楊婷婷 Yang, Ting-Ting |
|---|---|
| 論文名稱: |
類神經網路動態飛行參數驗證 Dynamic Flight Data Validation Using Artificial Neural Networks |
| 指導教授: |
陸鵬舉
Lu, Pong-Jeu |
| 學位類別: |
碩士 Master |
| 系所名稱: |
工學院 - 航空太空工程學系 Department of Aeronautics & Astronautics |
| 論文出版年: | 2007 |
| 畢業學年度: | 95 |
| 語文別: | 中文 |
| 論文頁數: | 141 |
| 中文關鍵詞: | 迴傳式類神經網路 、自相關類神經網路 |
| 外文關鍵詞: | Auto-Associative Neural Networks, Recurrent Neural Networks |
| 相關次數: | 點閱:96 下載:4 |
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本研究主旨在建立一動態飛行參數驗證程式。文中採用自相關類神經網路(Auto-Associative Neural Networks, AANN)作為程式發展的基礎,再加入迴傳式類神經網路(Recurrent Neural Networks, RNN)的觀念,發展出一套可驗證飛行參數的迴傳式自相關類神經網路(Recurrent AANN, R-AANN)。R-AANN可模擬飛行參數之間的動態關係,掌握各項參數隨時間的變化歷程及相互間關聯性,並透過此R-AANN以判斷各參數是否相容(Compatible)。為測試本網路的推廣能力,本文先藉由簡單的物理模型與非線性離散化模型來測試程式之可行性後,再使用於動態飛行參數上。為了方便後續的驗證,在此所使用之飛行參數是由飛行力學六自由度運動方程式(Six-Degree-of-Freedom Equations of Motion)所產生。結果顯示,本方法使用於動態飛行之縱向參數上有相當不錯之學習能力與相容性鑑定效果。
The objective of the present research is to develop a software system that can perform dynamic flight data validation using artificial neural networks. Auto-associative neural network (AANN) was adopted as the groundwork for method development. In order to strengthen the generalization ability of this AANN when coping with various dynamic situations that are not included in the training scenarios, recurrent neural network (RNN) was incorporated into this data validation AANN system. A newly constructed recurrent AANN (R-AANN) was thus obtained by combining together the characteristics associated with AANN and RNN. This R-AANN validity was first demonstrated using model problems consisting of a continuous spring-mass linear oscillator and a set of nonlinear discrete recurrence relationships. Longitudinal flight simulation was then conducted to generate the training and testing flight data. It was shown that both static AANN and dynamic R-AANN yield good data compatibility check ability of the parameters selected in the input node layer. However, R-AANN performance is superior in the validation of the underlying dynamics in terms of a better representation of the time derivatives of the flight parameters.
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