完整後設資料紀錄
DC 欄位 | 值 | 語言 |
---|---|---|
dc.contributor.author | 周品然 | en_US |
dc.contributor.author | ZHOU, PIN-RAN | en_US |
dc.contributor.author | 吳永春 | en_US |
dc.contributor.author | WU, YONG-CHUN | en_US |
dc.date.accessioned | 2014-12-12T02:11:04Z | - |
dc.date.available | 2014-12-12T02:11:04Z | - |
dc.date.issued | 1992 | en_US |
dc.identifier.uri | http://140.113.39.130/cdrfb3/record/nctu/#NT812327018 | en_US |
dc.identifier.uri | http://hdl.handle.net/11536/57204 | - |
dc.description.abstract | The estimate of aerodynamics parameters from fight data is very important for the analysis of the characteristics of an aircraft. In this thesis we use the Maximum Likeli-hod Estimate (MLE) method to identify the parameters of a simplified and linearized aircraft model with both the plant and measurement noises. An improvement has been made to make the Hessian matrix to be safely positive-definite. Simulations show that the proposed approach is applicable. | zh_TW |
dc.language.iso | zh_TW | en_US |
dc.subject | 飛機 | zh_TW |
dc.subject | 氣動力 | zh_TW |
dc.subject | 參數 | zh_TW |
dc.title | 飛機氣動力參數之判別 | zh_TW |
dc.title | Identification of aircraft areodynamics parameters | en_US |
dc.type | Thesis | en_US |
dc.contributor.department | 電控工程研究所 | zh_TW |
顯示於類別: | 畢業論文 |