Strong Tracking Unscented Kalman Filter for Identification of Inflight Icing

Aircraft icing degrades aerodynamic performance and poses safety risks, especially under nonlinear and uncertain conditions. In order to identify inflight icing in real time, this work proposes a Strong Tracking Unscented Kalman Filter (STUKF) which integrates the Unscented Kalman Filter (UKF) with...

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发表在:	Aerospace
Main Authors:	Huangdi Luo, Jianliang Ai
格式:	文件
语言:	英语
出版:	MDPI AG 2025-08-01
主题:	aircraft icing parameter identification unscented kalman filter strong tracking theory
在线阅读:	https://www.mdpi.com/2226-4310/12/9/779