Method for determining the altitude of an unknown space object to estimate the slant range in problems of orbit calculation from angular optical measurements

Authors

  • Vasilina S. Baranova Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus
  • Alexander A. Spiridonov Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus
  • Vladimir L. Kozlov Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus
  • Dmitrii V. Ushakov Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus
  • Vladimir A. Saetchnikov Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus

Keywords:

space object, optical measurements, orbital parameters

Abstract

A method for estimating the altitude of an unknown space object, assuming near-circular orbital motion, is presented. This technique is applied to adjust the slant range parameter and determine two position radius vectors based on optical angular measurements. The initial orbit determination approach utilises two radius vectors from correlated detection regions of the unknown satellite relative to a reference mask satellite. The orbital altitude for the two angular measurement regions of the detected Indefix/Ariane 42p satellite was determined with errors of 2.1 and 2.2 km respectively, compared to the calculated altitude of 752.2 km in the SGP model. By incorporating altitude-based corrections, the slant range error did not exceed 3 km. A comparative analysis was conducted on the initial orbit determination results for the Indefix/Ariane 42p satellite, evaluating the slant range through the projection of linear velocity onto the frame plane and using altitude-based corrections for slant range estimation.

Author Biographies

  • Vasilina S. Baranova, Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus

    researcher at the department of the physics and aerospace technologies, faculty of radiophysics and computer technology

  • Alexander A. Spiridonov, Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus

    PhD (physics and mathematics), docent; associate professor at the department of physics and aerospace technologies, faculty of radiophysics and computer technology

  • Vladimir L. Kozlov, Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus

    doctor of science (engineering), full professor; professor at the department of quantum radiophysics and optoelectronics, faculty of radiophysics and computer technology

  • Dmitrii V. Ushakov, Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus

    doctor of science (physics and mathematics), docent; dean of the faculty of radiophysics and computer technology

  • Vladimir A. Saetchnikov, Belarusian State University, 4 Niezaliezhnasci Avenue, Minsk 220030, Belarus

    doctor of science (physics and mathematics), full professor; head of the department of physics and aerospace technologies, faculty of radiophysics and computer technology

References

  1. Vallado DA. Fundamentals of astrodynamics and applications. 4th edition. Hawthorne: Microcosm Press; 2013. XXII, 1106 p. (Space technology library).
  2. Herrick S. Astrodynamics. Volume 1, Orbit determination, space navigation, celestial mechanics. London: Van Nostrand Reinhold Company; 1971. XXVI, 540 p.
  3. Escobal PR. Methods of orbit determination. Huntington: R. E. Krieger; 1976. XIX, 479 p.
  4. Battin RH. An introduction to the mathematics and methods of astrodynamics. Reston: American Institute of Aeronautics and Astronautics; 1999. XXXII, 799 p. (Przemieniecki JS, editor. AIAA education series).
  5. Bate RR, Mueller DD, White JE. Fundamentals of astrodynamics. New York: Dover Publications; 1971. XII, 455 p.
  6. Christian JA. Initial orbit determination from only heading measurements. Journal of Spacecraft and Rockets. 2023;60(4):1169–1175. DOI: 10.2514/1.A35593
  7. Kazemi S, Azad NL, Scott KA, Oqab HB, Dietrich GB. Orbit determination for space situational awareness: a survey. Acta Astronautica. 2024;222:272–295. DOI: 10.1016/j.actaastro.2024.06.015.
  8. Lei X, Wang K, Zhang P, Pan T, Li H, Sang J, et al. A geometrical approach to association of space-based very short-arc LEO tracks. Advances in Space Research. 2018;62(3):542–553. DOI: 10.1016/j.asr.2018.04.044.
  9. Fossà A, Armellin R, Delande E, Losacco M, Sanfedino F. A multifidelity approach to robust orbit determination. Acta Astronautica. 2024;214:277–292. DOI: 10.1016/j.actaastro.2023.10.040.
  10. Gronchi GF, Dimare L, Milani A. Orbit determination with the two-body integrals. Celestial Mechanics and Dynamical Astronomy. 2010;107(3):299–318. DOI: 10.1007/s10569-010-9271-9.
  11. Milani A, Gronchi GF, Vitturi MDM, Knežević Z. Orbit determination with very short arcs. I admissible regions. Celestial Mechanics and Dynamical Astronomy. 2004;90(1–2):57–85. DOI: 10.1007/s10569-004-6593-5.
  12. Cai H, Yang Y, Gehly S, Wu S, Zhang K. Improved tracklet association for space objects using short-arc optical measurements. Acta Astronautica. 2018;151:836–847. DOI: 10.1016/j.actaastro.2018.07.024.
  13. Bakhshiyan BT, Sukhanov AA, Fedyaev KS. Estimation of the determination accuracy of orbit parameters of the Apophis asteroid from measurement results. Cosmic Research. 2010;48(5):417–423. DOI: 10.1134/S0010952510050072.
  14. Mironov VV. A technique for estimating the space debris density from the data of onboard recording systems. Cosmic Research. 2003;41(3):204–208. DOI: 10.1023/A:1023395300193.
  15. Baranova V, Spiridonov A, Ushakov D, Kozlov V, Cherny V, Saetchnikov V. Geometric approach to determining the space object orbit altitude using angles-only measurements. In: Institute of Electrical and Electronics Engineers. Proceedings of 11th International workshop on metrology for aerospace; 2024 June 3–5; Lublin, Poland. [S. l.]: Institute of Electrical and Electronics Engineers; 2024. p. 173–177. DOI: 10.1109/MetroAeroSpace61015.2024.10591574.
  16. Baranova V, Spiridonov A, Ushakov D, Saetchnikov V. The resident space object detection method based on the connection between the Fourier domain image of the video data difference frame and the orbital velocity projection. Journal of Astronomy and Space Sciences. 2024;41(3):159–170. DOI: 10.5140/JASS.2024.41.3.159.
  17. Kovalevsky J, Seidelmann PK. Fundamentals of astrometry. Cambridge: Cambridge University Press; 2004. 422 p.
  18. Zhi Z, Qu H, Tao S, Zheng L, Ying Sh, Zhu H. The design of cone and pendulum scanning mode using dual-camera with multi-dimensional motion imaging micro-nanosatellite. Remote Sensing. 2022;14(18):4613–4641. DOI: 10.3390/rs14184613.
  19. Pineau D, Felicetti L. Design of an optical system for a Multi-CubeSats debris surveillance mission. Acta Astronautica. 2023;210:535–546. DOI: 10.1016/j.actaastro.2023.04.027.
  20. Баранова ВС, Спиридонов АА, Ушаков ДВ, Саечников ВА. Метод начального определения орбиты космического объекта по ограниченным данным угловых оптических измерений. Приборы и методы измерений. 2025;16(2):121–132. DOI: 10.21122/2220-9506-2025-16-2-121-132.
  21. Spiridonov A, Baranova V, Ushakov D, Saetchnikov V, Kenko Z, Zasmuzhats D, et al. University mobile optical surveillance system for low-Earth space object orbit determination. In: Institute of Electrical and Electronics Engineers. Proceedings of 9th International workshop on metrology for aerospace; 2022 June 27–29; Pisa, Italy. [S. l.]: Institute of Electrical and Electronics Engineers; 2022. p. 566–570. DOI: 10.1109/MetroAeroSpace54187.2022.9855955.
  22. Спиридонов АА, Баранова ВС, Саечников ВА, Ушаков ДВ. Моделирование построения региональной группировки наноспутников путем попутного запуска с различных космодромов. Журнал Белорусского государственного университета. Физика. 2022;2:50–59. DOI: 10.33581/2520-2243-2022-2-50-59.

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Published

2025-09-15

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Section

Research Instruments and Methods

How to Cite

(1)
Baranova, V. S. .; Spiridonov, A. A.; Kozlov, V. L.; Ushakov, D. V. .; Saetchnikov, V. A. Method for Determining the Altitude of an Unknown Space Object to Estimate the Slant Range in Problems of Orbit Calculation from Angular Optical Measurements. Журнал Белорусского государственного университета. Физика 2025, No. 2, 4-18.