Online Identification of Aircraft Model Parameters Based on Recursive Least Squares Method

In order to realize online update of the flight control system, online assessment of flight capability and online detection of an aircraft fault, the online identification method of unknown parameters in the aircraft dynamics model was studied. Firstly, based on the analysis of aircraft characterist...

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Bibliographic Details
Main Authors: JIANG Yongming, WANG Changqing, XU Cheng
Format: Article
Language:zho
Published: Editorial Office of Control and Information Technology 2019-01-01
Series:Kongzhi Yu Xinxi Jishu
Subjects:
Online Access:http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2096-5427.2019.04.010
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