On equilibrium positions bifurcations of Hamiltonian system in cases of double combined third order resonance

Theoretical mechanics


Аuthors

Holostova O. V.1*, Safonov A. I.2**

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. InfoSistem-35, 16, 3-Mytischinskaya str., bld. 37, Moscow, 129626, Russia

*e-mail: kholostova_o@mail.ru
**e-mail: lexafonov@mail.ru

Abstract

Motion of a near-autonomous time-periodic two-degree-of-freedom Hamiltonian system is considered near the trivial equilibrium position, stable in the linear approximation. The system is assumed to realize simultaneously two Raman third-order resonances being strong and weak. In this case, the frequencies of small oscillations are related also by the fourth-order resonant ratio. In the complete nonlinear system, this equilibrium position is unstable. By the perturbation theory methods, normalization of the Hamiltonian of the perturbed motion is performed in the members up to the fourth order inclusively with respect to disturbance, and account for the existing resonances. On the assumption that the summand coefficients related to the fourth-order resonance are small, the approximate (model) system, dependent on the three parameters, was considered. The issue of existence and number of equilibrium positions of the model system was solved by analytical and graphics methods. The domains, where the number of equilibrium positions of the model system can vary from zero to five were identified in the space of parameters of the problem.

As an application, the problem of motion of a dynamically symmetric satellite (modeled by a rigid body) about the center of mass in the central Newtonian gravitational field on the orbit with small eccentricity was considered. The satellite motion was studied near its periodic motion, emerging from the hyperboloid precession on a circular orbit. For parameter values, corresponding to the multiple Raman third-order resonance, the coefficients of the normal forms of the model system are found. It was shown, that there are three equilibrium points in this system, two of which are unstable and the third stable in the linear approximation.

Keywords:

Hamiltonian system, multiple Raman resonance, dynamically symmetric satellite, hyperboloid precession

References

  1. Kunitsyn A.L. Differentsial’nye uravneniya, 1971, vol. 7, no. 9, pp. 1704 – 1706.

  2. Khazina G.G. Prikladnaya matematika i mekhanika, 1974, vol. 3, no. 1, pp. 56 – 65.

  3. Kunitsyn A.L., Medvedev S.V. Prikladnaya matematika i mekhanika, 1977, vol. 41, no. 3, pp. 422 – 429.

  4. Kunitsyn A.L., Tashimov L.T. Nekotorye zadachi ustoichivosti nelineinykh rezonansnykh sistem (Some stability problems of nonlinear resonant systems), Alma-Ata, Gylym, 1990, 196 p.

  5. Khazin L.G. Ob ustoichivosti polozheniya ravnovesiya gamil’tonovykh sistem differentsial’nykh uravnenii (Vzaimodeistvie rezonansov tret’ego poryadka) (On stability of an equilibrium position of Hamiltonian systems of differential equations (Third-order resonance interaction), Institut prikladnoi matematiki AN SSSR, preprint no. 133, Moscow, 1981, 20 p.

  6. Khazin L.G. Interaction of third-order resonances in problems of the stability of hamiltonian systems, Journal of applied mathematics and mechanics, 1984, vol. 48, issue 3, pp. 356 – 380.

  7. Markeev A.P. On a Multiple Resonance in Linear Hamiltonian Systems, Doklady Physics, 2005, vol. 50, no. 5, pp. 278 – 282.

  8. Markeev A.P. Multiple parametric resonance in Hamilton systems, Journal of applied mathematics and mechanics, 2006, vol. 70, no. 2, pp. 176 – 194.

  9. Markeev A.P. Lineinye gamil’tonovy sistemy i nekotorye zadachi ob ustoichivosti dvizheniya sputnika otnositel’no tsentr mass (Linear Hamiltonian systems and some problems of a satellite movement around a center of mass), Moscow – Izhevsk, Institut komp’yuternykh issledovanii, 2009, 396 p.

  10. Markeev A.P. On One Special Case of Parametric Resonance in Problems of Celestial Mechanics, Astronomy Letters, 2005, vol. 31, no.5, pp. 350 – 356.

  11. Markeev A.P. Multiple Resonance in One Problem of the Stability of the Motion of a Satellite Relative to the Center of Mass, Astronomy Letters, 2005, vol. 31, no. 9, pp. 627 – 633.

  12. Kholostova O.V. Nelineinaya dinamika, 2012, vol. 8, no. 2, pp. 267 – 288.

  13. Kholostova O.V. Nelineinaya dinamika, 2015, vol. 11, no. 4, pp. 671 – 683.

  14. Kholostova O. Stability of triangular libration points in a planar restricted elliptic three body problem in cases of double resonances, International Journal of Non-Linear Mechanics, 2015, vol. 73, pp. 64 – 68.

  15. Kholostova O.V. Zadachi dinamiki tverdykh tel s vibriruyushchim podvesom (The problems of rigid bodies dynamics with vibrating suspension point), Moscow – Izhevsk, Institut komp’yuternykh issledovanii, 2016, 308 p.

  16. Kholostova O.V. Trudy XI Mezhdunarodnoi Chetaevskoi konferentsii. Kazan’, KNITU-KAI, 2017, vol. 2, pp. 222 – 229.

  17. Safonov A.I., Kholostova O.V. Vestnik Udmurtskogo universiteta. Matematika. Mekhanika. Komp’yuternye nauki, 2016, vol. 26, no. 3, pp. 418 – 438.

  18. Bardin B.S., Savin A.A. Trudy MAI, 2016, no. 85, available at: http://trudymai.ru/eng/published.php?ID=65212

  19. Bardin B.S., Chekina E.A. Trudy MAI, 2016, no. 89, available at: http://trudymai.ru/eng/published.php?ID=72568

  20. Beletskij V.V. Dvizhenie sputnika otnositel’no centra mass v gravitacionnom pole (Satellite motion around the center of mass in gravitational field), Moscow, Izd-vo MGU, 1975, 308 p.

  21. Duboshin G.N. Bjulleten’ ITA AN SSSR, 1960, no. 7, pp. 511 – 520.

  22. Chernous’ko F.L. On the stability of regular precession of a satellite, Journal of applied mathematics and mechanics, 1964, vol. 28, no. 1, pp. 181 – 184.

  23. Sarychev V.A. Kosmicheskie isssledovanija, 1965, vol. 3, no. 5, pp. 667 – 673.


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