A study on the efficiency of methods for the calculation of intermediate perturbed orbit from range and range rate measurements at three times
UDC
521.3EDN
RUBBRDAbstract
Two methods that the author developed for finding the orbit of a small celestial body from three pairs of range and range rate observations are applied to the determination of orbits of some artificial Earth satellites. The efficiency of using these methods is investigated in comparison with the commonly used procedure based on the construction of the unperturbed Keplerian orbit. The comparison shows that the methods proposed are an efficient means for studying perturbed motion.
Keywords:
preliminary orbit determination, intermediate perturbed orbit, dynamics of artificial Earth satellitesFunding information
Работа выполнена при финансовой поддержке РФФИ (проект № 12-02-00220-а).
References
- Baker R.M.L., Makemson M.W. An Introduction to Astrodynamics. New York: Academic Press, 1967. 439 p.
- Roy A.E. Orbital Motion. Bristol: IOP Publishing, 2005. 526 p.
- Шефер В.А. Метод определения промежуточной орбиты по измерениям дальности и скорости ее изменения в три момента времени // Изв. вузов. Физика. 2012. Т. 55. № 10/2. С. 11-18.
- Шефер В.А. Метод высокоточного определения орбиты по измерениям дальности и скорости ее изменения в три момента времени // Современная баллистика и смежные вопросы механики: Материалы Всерос. науч. конф., г. Томск, 17-19 ноября 2009 г. Томск, 2010. С. 326-328.
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Dates
Submitted
October 7, 2013
Accepted
October 9, 2013
Published
December 30, 2013
How to Cite
[1]
Shefer, V.A., A study on the efficiency of methods for the calculation of intermediate perturbed orbit from range and range rate measurements at three times. Ecological Bulletin of Research Centers of the Black Sea Economic Cooperation, 2013, № 4, pp. 167–170.
License
Copyright (c) 2013 Шефер В.А.
This work is licensed under a Creative Commons Attribution 4.0 International License.
