ACCURACY OF ORBITS OF SMALL CELESTIAL BODIES OBTAINED USING DIFFERENT SOFTWARE
Section: CELESTIAL MECHANICS AND ASTROMETRY
Authors:
1.
Institute of Applied Astronomy of the Russian Academy of Sciences
2.
Institute of Applied Astronomy, Russian Academy of Sciences
3.
Tomsk State University
4.
Tomsk State University
Type:
Сonference article
Published:
27.12.2024
Subject area:
UDC 52
UDC 53
UDC 520
UDC 521
UDC 523
UDC 524
UDC 52-1
UDC 52-6
CSCSTI 41.00
CSCSTI 29.35
CSCSTI 29.31
CSCSTI 29.33
CSCSTI 29.27
CSCSTI 29.05
Russian Classification of Professions by Education 03.06.01
Russian Classification of Professions by Education 03.05.01
Russian Classification of Professions by Education 03.04.03
Russian Library and Bibliographic Classification 2
Russian Library and Bibliographic Classification 223
Russian Trade and Bibliographic Classification 614
Russian Trade and Bibliographic Classification 6135
BISAC SCI004000 Astronomy
BISAC SCI005000 Physics / Astrophysics
UDC 53
UDC 520
UDC 521
UDC 523
UDC 524
UDC 52-1
UDC 52-6
CSCSTI 41.00
CSCSTI 29.35
CSCSTI 29.31
CSCSTI 29.33
CSCSTI 29.27
CSCSTI 29.05
Russian Classification of Professions by Education 03.06.01
Russian Classification of Professions by Education 03.05.01
Russian Classification of Professions by Education 03.04.03
Russian Library and Bibliographic Classification 2
Russian Library and Bibliographic Classification 223
Russian Trade and Bibliographic Classification 614
Russian Trade and Bibliographic Classification 6135
BISAC SCI004000 Astronomy
BISAC SCI005000 Physics / Astrophysics
Language:
English
Keywords:
small celestial bodies; dynamics; orbit improvement; asteroid/comet hazard
Abstract (English):
The threat of a collision with a potentially hazardous object (PHO) and smaller asteroids requires the ability to reliably calculate the orbits of celestial bodies. The quality of the determined orbit depends on both the accuracy and intervals of observations and on the method of their processing: the completeness of the dynamic model, the method of numerical integration, calculation errors, etc. The practical implementation of the orbit determination algorithm is associated with the peculiarities of taking into account the above factors. To assess the accuracy of motion prediction using orbits obtained with the help of different software packages, we compared the deviations in observed and calculated values of observations, i.e. $O$–$C$, that were not included in the orbit improvement. The $O$–$C$ comparison was carried out for orbits obtained using software developed in leading Russian scientific organizations with teams working on asteroid-comet dynamics: Pulkovo, Tomsk State University (TSU) and Institute of Applied Astronomy of RAS (IAA), as well as orbits presented on the Jet Propulsion Laboratory's (JPL) Horizons website. The asteroids Apophis and Phaethon were chosen as objects for which the $O$–$C$ comparison was performed. Observations of each asteroid were divided into two samples by time. The asteroid's orbit was improved using the earlier sample, and the later sample was used to access the accuracy of the prediction. The $O$–$C$ distribution profile for orbits obtained using different software turned out to be very similar, indicating the proximity of predictions. The most accurate orbits were obtained using the Improvement and IDA software developed at the IAA and TSU, respectively.
The threat of a collision with a potentially hazardous object (PHO) and smaller asteroids requires the ability to reliably calculate the orbits of celestial bodies. The quality of the determined orbit depends on both the accuracy and intervals of observations and on the method of their processing: the completeness of the dynamic model, the method of numerical integration, calculation errors, etc. The practical implementation of the orbit determination algorithm is associated with the peculiarities of taking into account the above factors. To assess the accuracy of motion prediction using orbits obtained with the help of different software packages, we compared the deviations in observed and calculated values of observations, i.e. $O$–$C$, that were not included in the orbit improvement. The $O$–$C$ comparison was carried out for orbits obtained using software developed in leading Russian scientific organizations with teams working on asteroid-comet dynamics: Pulkovo, Tomsk State University (TSU) and Institute of Applied Astronomy of RAS (IAA), as well as orbits presented on the Jet Propulsion Laboratory's (JPL) Horizons website. The asteroids Apophis and Phaethon were chosen as objects for which the $O$–$C$ comparison was performed. Observations of each asteroid were divided into two samples by time. The asteroid's orbit was improved using the earlier sample, and the later sample was used to access the accuracy of the prediction. The $O$–$C$ distribution profile for orbits obtained using different software turned out to be very similar, indicating the proximity of predictions. The most accurate orbits were obtained using the Improvement and IDA software developed at the IAA and TSU, respectively.
Keywords:
small celestial bodies; dynamics; orbit improvement; asteroid/comet hazard
small celestial bodies; dynamics; orbit improvement; asteroid/comet hazard
1. Galushina T., Letner O., 2021, Astronomical and Astrophysical Transactions, 32., 4, p. 355
2. Gehrels T., 1994, Tucson: University of Arizona Press
3. Moyer T., 1971, Technical Report 32-1527, NASA/JPL
4. Reddy V., Kelley M., Benner L., et al., 2024, Planetary Science Journal, 5, p. 141
