Use of GNSS-Based Pseudo-Acceleration Measurements and Orbital Constraints to Initialize Spaceborne Receiver Orbit Solutions
LAURICHESSE, D., GRATTON, S., MERCIER, F., TOURNIER, T., BERTHIAS, J. P., ISSLER, J. L., DOLISZNY, F., REVIDON, P.Том:
50
Мова:
english
Журнал:
Navigation
DOI:
10.1002/j.2161-4296.2003.tb00321.x
Date:
June, 2003
Файл:
PDF, 133 KB
english, 2003