High-precision trajectory determinations of low orbital space vehicles using the signals from the GNSS global navigation satellite system
|1Zhalilo, AA, 2Khomyakov, EN, 3Flerko, SN, 4Volokh, KF |
1Main Astronomical Observatory of the National Academy of Sciences of Ukraine, Kyiv, Ukraine; Kharkіv National University of Radio Electronics of the Ministry of Education and Science of Ukraine, Kharkiv,Ukraine
2National Aerospace University “'Kharkiv Aviation Institute”, Kharkiv, Ukraine
3I. Kozhedub Kharkiv Air Force University, Kharkiv, Ukraine
4State Space Agency of Ukraine, Kyiv, Ukraine
|Kosm. nauka tehnol. 1999, 5 ;(2):93–102|
|Publication Language: Russian|
We propose and analyze several variants of organizing high-precision determination of low-orbital space vehicle trajectory parameters by the use of the GNSS global navigation satellite system. We also consider the peculiarities of realization and the accuracy of trajectory determination from the results of the joint processing of code and phase measurements made on board space vehicles and by the GNSS ground reference station network.
|Keywords: code and phase measurements, GNSS, low orbital space vehicles|
21. Zhalilo A. A., Yakovchenko A. I. The realization technique and features of the GPS/GLONASS relative geodetic adjustment using float solution. Proc. 2nd European Symp. on GNSS'98, Toulouse, France, October 23—25, 1998, Vol. 2. IX-P-02, P. 1—5 (1998).