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dc.contributor.author周品然en_US
dc.contributor.authorZHOU, PIN-RANen_US
dc.contributor.author吳永春en_US
dc.contributor.authorWU, YONG-CHUNen_US
dc.date.accessioned2014-12-12T02:11:04Z-
dc.date.available2014-12-12T02:11:04Z-
dc.date.issued1992en_US
dc.identifier.urihttp://140.113.39.130/cdrfb3/record/nctu/#NT812327018en_US
dc.identifier.urihttp://hdl.handle.net/11536/57204-
dc.description.abstractThe 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.isozh_TWen_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.titleIdentification of aircraft areodynamics parametersen_US
dc.typeThesisen_US
dc.contributor.department電控工程研究所zh_TW
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