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Information Fusion Based on Complementary Filter for SINS/CNS/GPS Integrated Navigation System of Aerospace Plane

In order to solve the problems of heavy computational load and poor real time of the information fusion method based on the federated Kalman filter (FKF), a novel information fusion method based on the complementary filter is proposed for strapdown inertial navigation (SINS)/celestial navigation sys...

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Detalles Bibliográficos
Autores principales:	Zhao, Yanming, Yan, Gongmin, Qin, Yongyuan, Fu, Qiangwen
Formato:	Online Artículo Texto
Lenguaje:	English
Publicado:	MDPI 2020
Materias:	Article
Acceso en línea:	https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7765422/ https://www.ncbi.nlm.nih.gov/pubmed/33333963 http://dx.doi.org/10.3390/s20247193

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