State-estimation and parameter identification of freely-spinning rigid spacecraft
(1976) International Journal of Systems Science — Vol. 7, n° 12, p. 1377-1386 (1976)
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- Abstract
- The attitude estimation of a rigid spacecraft from the noise-corrupted measures provided by sensors is studied. The method used is based on the EKF algorithm and, due to the lack of precision that can exist on the values of certain parameters, an augmented state-vector comprising these parameters must be considered. The filter then provides an estimation of these parameters along with the original state-variables of the system. The method is implemented using simulated model.
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Citations
Johnson, D. (1976). State-estimation and parameter identification of freely-spinning rigid spacecraft. International Journal of Systems Science, 7(12), 1377-1386. https://hdl.handle.net/2078.5/149217 (Original work published 1976)