飛機氣動力參數之判別

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