Calcolo di orbile a mezzo di misura di distanze 2°
Main Article Content
Abstract
L'autore presenta, in questa nota, un metodo per la
determinazione di orbite di satelliti attraverso l'elaborazione di sole misure
di distanza.
Nella prima parte del lavoro è illustrata la procedura matematica.
Nella parte successiva sono analizzati i risultati numerici ottenuti
simulando misure di distanza per diverse configurazioni osservatore-satellite.
Tali risultati si dimostrano più che soddisfacenti in quanto determinano la
posizione dell'osservatore e l'orbita del satellite con un errore relativo
dell'ordine di IO-8.
SUMMARY. — The author presents, in this note, a method for the determination
of satellite orbits only through the elaboration of range measurements.
The mathematical procedure is illustreted in the first part of the paper.
The numerical results obtained by simulating range measurements of
several observer-satellite configurations are analyzed in the subsequent part
of the paper. The results are very satisfactory since the parameters, which
determine the observer position and the satellite orbit, are obtained with a
relative error of about 10-8.
determinazione di orbite di satelliti attraverso l'elaborazione di sole misure
di distanza.
Nella prima parte del lavoro è illustrata la procedura matematica.
Nella parte successiva sono analizzati i risultati numerici ottenuti
simulando misure di distanza per diverse configurazioni osservatore-satellite.
Tali risultati si dimostrano più che soddisfacenti in quanto determinano la
posizione dell'osservatore e l'orbita del satellite con un errore relativo
dell'ordine di IO-8.
SUMMARY. — The author presents, in this note, a method for the determination
of satellite orbits only through the elaboration of range measurements.
The mathematical procedure is illustreted in the first part of the paper.
The numerical results obtained by simulating range measurements of
several observer-satellite configurations are analyzed in the subsequent part
of the paper. The results are very satisfactory since the parameters, which
determine the observer position and the satellite orbit, are obtained with a
relative error of about 10-8.
Article Details
How to Cite
BOTTI, C. (1976) “Calcolo di orbile a mezzo di misura di distanze 2°”, Annals of Geophysics, 29(1-2), pp. 89–120. doi: 10.4401/ag-4795.
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