Unscented Kalman filter applied to the spacecraft attitude estimation with Euler angles

DOI10.1155/2012/985429zbMath1264.93245OpenAlexW2018864026WikidataQ58912800 ScholiaQ58912800MaRDI QIDQ1955439

Roberta Veloso Garcia, Hélio Koiti Kuga, Maria Cecília F. P. S. Zanardi

Publication date: 11 June 2013

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2012/985429

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Signal theory (characterization, reconstruction, filtering, etc.) (94A12)

Related Items (1)

Kalman filter for attitude determination of a cubesat using low-cost sensors

Cites Work

• Unnamed Item

This page was built for publication: Unscented Kalman filter applied to the spacecraft attitude estimation with Euler angles