The theory of nonlinear filtering has been applied to the problem of the attitude determination of a satellite. Two approximation methods have been studied with a view to practical implementation. Computer simulation results are included.
Attitude Determination Via Nonlinear Filtering
IEEE Transactions on Aerospace and Electronic Systems ; AES-5 , 6 ; 906-911
01.11.1969
1323953 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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