Fully Multiplicative Unscented Kalman Filter for Attitude Estimation
Recommended Citation
R. Zanetti and K. J. De Mars, "Fully Multiplicative Unscented Kalman Filter for Attitude Estimation," Journal of Guidance, Control, and Dynamics, vol. 41, no. 5, pp. 1181 - 1187, American Institute of Aeronautics and Astronautics, Jan 2018.
The definitive version is available at https://doi.org/10.2514/1.G003221
Department(s)
Mechanical and Aerospace Engineering
Publication Status
Full Access
International Standard Serial Number (ISSN)
1533-3884; 0731-5090
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2024 American Institute of Aeronautics and Astronautics, All rights reserved.
Publication Date
01 Jan 2018
