Dynamic Error Suppression of Inertial Measurement Unit Based on Improved Unscented Kalman Filter

In this paper， an algorithm on measurement noise with adaptive strong tracking unscented Kalman filter （ASTUKF） is advanced to improve the precision of pose estimation and the stability for data computation. To suppress high-frequency noise， an infinite impulse response filter （IIRF） is introduced a...

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Bibliografiska uppgifter

Huvudupphov:	LI Na, LI Kun, HE Haiyu, JING Min
Materialtyp:	Artigo
Språk:	Inglês
Utgiven:	Editorial Office of Transactions of Nanjing University of Aeronautics and Astronautics 2025-12-01
Serie:	Transactions of Nanjing University of Aeronautics and Astronautics
Ämnen:	accelerometer inertial measurement unit adaptive strong tracking unscented kalman filter（astukf） quaternion kalman filter
Länkar:	https://tnuaa.nuaa.edu.cn/njhkhten/article/html/202506012?st=article_issue
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