NASA has proposed to put a Space Station in orbit in the early 1980s. This paper describes the steps involved in applying maximum likelihood estimation (MLE) method to indentify the parameters of the dynamic model of thr Space Station. The amount of computation in the MLE approach is reduced by using the method of successive approximation. Numerical results based on simulated data is presented in the paper.
Indentification of Space Station Dynamics
Indentifizierung des dynamischen Verhaltens von Raumstationen
Proc. of the 24th IEEE Conf. on Decision and Control ; 2 ; 1264-1265
1985
2 Seiten, 3 Bilder, 1 Tabelle, 3 Quellen
Conference paper
English
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