Performance evaluation of a central difference Kalman filter applied to attitude determination

Author:

Baroni LeandroORCID,Kuga Hélio K.,Garcia Roberta V.,Silva William R.,Zanardi Maria Cecília,Pardal Paula C. P. M.

Funder

Conselho Nacional de Desenvolvimento Científico e Tecnológico

Publisher

Springer Science and Business Media LLC

Subject

Physical and Theoretical Chemistry,General Physics and Astronomy,General Materials Science

Reference27 articles.

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2. T. Villela, C.A. Costa, A.M. Brandão, F.T. Bueno, R. Leonardi, Towards the thousandth CubeSat: A statistical overview. Int. J. Aerosp. Eng. 2019, 5063145 (2019). https://doi.org/10.1155/2019/50631455063145

3. V. Lundén, T. Peltola, P. Niemelä, K. Cheremetiev, B. Clayhills, M. Palmroth, E. Kilpua, R. Vainio, P. Janhunen, J. Praks, Performance and design of commercial off-the-shelf (COTS) components-based magnetometer for FORESAIL-1 CubeSat. In: Small Satellites, System & Services Symposium, Vilamoura, Portugal (2022)

4. F.L. Markley, Attitude determination using two vector measurements. Nasa: Goddard Space Flight Center (1998). https://ntrs.nasa.gov/citations/19990052720

5. M.D. Shuster, S.D. Oh, Three-axis attitude determination from vector observations. J. Guidance Control 4(1), 70–77 (1981)

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1. Celestial mechanics: new discoveries and challenges for space exploration;The European Physical Journal Special Topics;2023-12

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