A Maneuver of Escape from the Vicinity of a Collinear Libration Point Using Light Pressure Forces

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Abstract

The orbital motion of a spacecraft with a solar sail in the vicinity of the Sun–Earth collinear libration point is studied. The study is carried out within the Hill approximation of the circular restricted three-body problem. The collinear libration point is unstable, but instability can be a positive factor in the tasks of maneuvering in interplanetary space. This is because a small change in velocity near an unstable libration point can lead to a significant change in orbital motion. This property can be used in the development of projects to counteract the comet–asteroid hazard. A scheme for constructing the trajectories of interception of a spacecraft with a potentially hazardous object is proposed. One of the stages of this scheme, an optimal escape from the vicinity of the libration point using light pressure forces, is considered. The results of numerical simulations are presented.

About the authors

D. V. Shymanchuk

St. Petersburg State University, 198504, St. Petersburg, Russia

Email: d.shimanchuk@spbu.ru
Россия, Санкт-Петербург

A. S. Shmyrov

St. Petersburg State University, 198504, St. Petersburg, Russia

Email: d.shimanchuk@spbu.ru
Россия, Санкт-Петербург

V. A. Shmyrov

St. Petersburg State University, 198504, St. Petersburg, Russia

Author for correspondence.
Email: d.shimanchuk@spbu.ru
Россия, Санкт-Петербург

References

  1. Кериорри, Куартьеллез (M. Ceriorry and J.P.S. Cuartiellez), Proceed. of 64th Inter. Astronautical Congress, Beijing, China. Paper IAC-13-C1.4.3 (2013).
  2. Маркеев А.П., Точки либрации в небесной механике и космодинамике (М.: Наука, 1978).
  3. Поляхова и др. (E. Polyakhova, A. Shmyrov, and V. Shmyrov), AIP Conf. Proceed. (Ed. E.V. Kustova, G.A. Leonov, M.P. Yushkov, N.F. Morosov, M.A. Mekhonoshina, St. Petersburg, AIP, 2018).
  4. Пупков и др. (M.V. Pupkov, N.A. Eismont, K.S. Fedyaev, and V.A. Zubko), 17th Inter. Conf. on Space Operations, SpaceOps-2023, ID # 357 (2023).
  5. Сюняев Р.А. и др., Письма в Астрон. журн. 48, 301 (2022).
  6. Фаркуар и др. (R.W. Farquhar, D.P. Muhonen, and D.L. Richardson), J. Spacecraft and Rockets 14, 170 (1977).
  7. Шиманчук Д.В., Вестн. СПбГУ. Сер. 10: Прикладная математика, информатика, процессы управления. 13, 147 (2017).
  8. Шиманчук Д.В., Шмыров А.С., Шмыров В.А., Письма в Астрон. журн. 46, 193 (2020) [D.V. Shimanchuk et al., Astron. Lett. 46, 185 (2020)].
  9. Шиманчук Д.В., Шмыров А.С., Шмыров В.А., Письма в Астрон. журн. 47, 733 (2021) [D.V. Shymanchuk et al., Astron. Lett. 47, 710 (2021)].
  10. Шиманчук Д.В., Шмыров А.С., Шмыров В.А., Письма в Астрон. журн. 48, 592 (2022) [D.V. Shymanchuk et al., Astron. Lett. 48, 469 (2022)].
  11. Шмыров В.А., Вестн. СПбГУ. Сер. 10. Прикладная математика. Информатика. Процессы управления. 2, 193 (2005).
  12. Шмыров, Шиманчук (A. Shmyrov and D. Shymanchuk), 2015 Inter. Conf. on Mechanics — Seventh Polyakhov’s Reading (Ed. A.A. Tikhonov, St. Petersburg, IEEE, 2015).
  13. Шмыров и др. (A. Shmyrov, D. Shymanchuk, and L. Sokolov), 2015 Inter. Conf. on ‘‘Stability and Control Processes’’ in Memory of V.I. Zubov, SCP 2015 — Proceed. (Ed. L.A. Petrosyan, A.P. Zhabko, St. Petersburg, IEEE, 2015), p. 129.
  14. Эйсмонт Н.А., Боярский М.Н., Ледков А.А., Назиров Р.Р., Данхэм Д.У., Шустов Б.М., Астрон. вестник. 47, 352 (2013).

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