On the calculation of orbits of spacecrafts equipped with receiving devices GLONASS/GPS
About authors
- 1 — Saint Petersburg Military Engineering-Technical University
- 2 — Saint Petersburg Military Engineering-Technical University
- 3 — Saint Petersburg Military Engineering-Technical University
Abstract
The main question of using GPS/GLONASS receivers for satellite orbit determitations are given. The "a priori'' calculations of satellite orbit accuracy are done. The investigation results may be applied in designing perspective cosmic geodetic apparatus.
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