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Journal of computer & systems sciences international, 2020-05, Vol.59 (3), p.430-450
Ort / Verlag
Moscow: Pleiades Publishing
Erscheinungsjahr
2020
Link zum Volltext
Quelle
SpringerLink (Online service)
Beschreibungen/Notizen
Methods and algorithms for determining the orbit of a space vehicle onboard using the measurements of global navigation satellite (NS) systems are considered. Methods and algorithms for obtaining radio navigation measurements in the case of the highly dynamic orbital motion are described. The celestial mechanics interpretation of measurements is given. Algorithms for the three-phase processing of trajectory measurements that improve the reliability and accuracy of determining the orbit are proposed. A mathematical model of a simulator of the satellite navigation signals is developed. The computational results are presented.