Non-linear parametric resonance driven oscillations of dumbell satellite in elliptical orbit under the combined effects of magnetic field of the earth and oblateness of the earth

  • Authors

    • A. Narayan
    • M. D. Pandey BIT DURG
    2015-01-02
    https://doi.org/10.14419/ijaa.v3i1.3897
  • Evolutional and Non-Evolutional, Perturbing Forces, Stability.
  • Parametric resonance driven oscillations of a dumbbell satellite in elliptical orbit in central gravitational field of force under the combined effects of perturbing forces Earth Magnetic field and Oblateness of the Earth has been studied. The system comprises of two satellite connected by a light, flexible and inextensible cable, moves like a dumbbell satellite in elliptical orbit, in central gravitational field of force. The gravitational field of the Earth is the main force governing the motion and magnetic field of the Earth and Oblateness of the Earth are considered to be perturbing forces, disturbing in nature. Non-linear oscillations of dumbbell satellite about the equilibrium position in the neighborhood of parametric resonance \(w=1/2\), under the influence of perturbing forces, which is suitable for exploiting the asymptotic methods of Bogoliubov, Krilov and Metropoloskey has been studied, considering ‘e’ to be a small parameter. The Hamiltonian has been constructed for the problem and phase analysis has been applied to investigate the stability of the system.

  • References

    1. [1] Beletsky, V.V. (1969), about the relative motion of two connected bodies, Kosmichekiya Isseldovania, 827-840, In Russian.

      [2] Beletsky, V.V., Levin, E.M. (1993), Dynamics of space tether systems, Advances of the Astronomical Sciences, 83, 267-322.

      [3] Beletsky, V.V., Novikova, E.T. (1969), about the relative motion of two connected bodies, Kosmichekiya Isseldovania, 7 377-384, In Russian.

      [4] Bogoliubov, N.N., Mitropolosky, Y.A. (1961), asymptotic methods in the theory of non-linear oscillations, Hindustan publishing company Delhi 06.

      [5] Celletti, Alessandria, Vladislov, V. Sidorenko. (2008), some properties of dumbbell satellite altitude dynamics, Celest. Mech. & Dyn. Astro, 105-126.

      [6] Das, S.K., Bhattacharya, P.K., Singh, R.B. (1976), Effects of magnetic force on the motion of system of two cable connected satellite in orbit, Proc. Nat. Acad. Sci. India, 287-299.

      [7] Khan, Ayub, Goel, Neeti. (2011), Chaotic motion in problem of dumbell satellite, International journal comtemp. Maths sciences vol.6, 299-307.

      [8] Krupa, M., Kuha, A., Poth W., Schagrl, M., Stiensl, A., Steiner, W., Treger, H., Wiedermann, G. (2000), Tethered satellite systems: A new concept of space flight, European Journal of Mechanics. A Solid 19 – Special Issue, S145-S164.

      [9] Krupa, M., Poth, W., Schagrl, M., Stiensl, A., Steiner, W., Treger, H., Wiedermann, G. (2006), Modelling, dynamics and central of tethered satellite systems, Non -linear Dynamics, 73-96. http://dx.doi.org/10.1007/s11071-006-0752-z.

      [10] Liapunov, A.M. The general problem of stability of motion, Sobrania Sachimediviya, 2, In Russian.

      [11] Langbort, Cedric. (2002), Bifurcation of relative equilibria in the main problem of artificial satellite theory for a prolate orbit, Celestial Mechanics & Dynamical Astronomy, 369- 385. http://dx.doi.org/10.1023/A:1021185011071.

      [12] Markeev, A.P., (2003), Bardin, B.S. On the stability of planar oscillations and rotation of a satellites in circular orbit, Celestial Mechanics & Dynamical Astronomy, 57-66.

      [13] Mishra, A.K., Modi, V. J. (1982), Deponent and retrieval of shuttle supported tethered satellites Journal of Guidance and Central, 5, No. 3, 278- 285.

      [14] Narayan, A., Singh, R.B. (1987), Non-linear non-resonance oscillation of interconnected satellites system under the solar pressure about the position of equilibrium for small eccentricity, Proc. Nat. Acad. Sci., India, 427-437.

      [15] Narayan, A., Singh, R.B. (1990), Non-linear main resonance oscillation of the system of two interconnected satellites under the influence of solar pressure about stable equilibrium for small eccentricity, Proc. Nat. Acad. Sci., India, 307-313.

      [16] Narayan, A., Singh, R.B. (1992), Non-linear parametric resonance oscillation of the system of two interconnected satellites under the influence of solar pressure about the stable position of equilibrium, Proc. Nat. Acad. Sci., India vol.63 A.

      [17] Narayan, A., Srivastav, S., Dewangan, S. (2004), Effects of earth magnetic field on the stability of cable connected satellites system in equatorial orbit, Journal of AMSE modelling B, 45-60.

      [18] Narayan, A., Pandey, M.D. (2010), Condition of free and constrained motion of cable connected satellites system in low altitude orbit, IJPAM Bulgaria, 107-127.

      [19] Narayan, A., Pandey, M.D. (2011), Condition of non-linear stability of dumbell satellite in elliptical orbit. IJPAM Bulgaria, 173-194.

      [20] Narayan, A., Pandey, M.D., and Narayan, Amitesh. (2012), some non-linear resonance oscillations of dumbell satellite in elliptical orbit. IJPAM Bulgaria, 931-944.

      [21] Nechville's, V. (1926), Surune Nouvelle formed equations differentials due problem restraint elliptique comptc rendus, Acad. Paris, Compt. Rend. 182- 3100.

      [22] Palacian, J.F. (2007), Dynamics of a satellites orbiting a planet with an inhomogeneous gravitational field, Celestial Mechanics & Dynamical Astronomy, 219-249. http://dx.doi.org/10.1007/s10569-007-9078-5.

      [23] Sarychev, V.A., Mirer, S.A. (2000), Relative equilibria of a satellites subjected to gravitational and arodynamics torque's, Celestial Mechanics& Dynamical Astronomy 76, 55-68. http://dx.doi.org/10.1023/A:1008389730047.

      [24] Sarychev, V.A., Mirer, S.A. Degtyarev, A.A., Durate, E.K. (2007), Investigation equilibria of a satellite subjected to gravitational and aerodynamic torques, Celestial Mechanics & Dynamical Astronomy, 267-287. http://dx.doi.org/10.1007/s10569-006-9064-3.

      [25] Sharma, S., Narayan, A. (2001), Non-linear oscillation of inter connected satellite system under the combined influence of the solar radiation pressure and dissipative forces general nature, Bull. Astronomical Soc. India, 29.

      [26] Sharma, S., Narayan, A. (2002), Effect of solar radiation pressure on the motion and stability of inter connected satellites system in orbit, Indian J. Pure Appl. Math., 33, No. 5, 609-623.

      [27] Singh, R.B. (1971), Three dimensional motion of two-connected bodies in the central gravitational field of force, In Problem of Guided Motion in Mechanics, Russian Collection, 210-215.

      [28] Singh, R.B. (1973), three dimensional motion of a system of two cables connected satellites in orbit, Astronautica Acta, 19, 301-308.

      [29] [29] Singh, B.M., Narayan, A., Singh, R.B. (1997), Non-linear parametric resonance oscillation of the system of two interconnected satellites orbiting around an oblate Earth, Proc. Nat. Acad. Sci., India, 67A, 45-55.

      [30] Singh, B.M., Narayan, A., Singh, R.B. (2001), Non-linear effects in the motion and stability of an inter connected satellites system orbiting around an oblate Earth, Proc. Nat. Acad. Sci., India, 71, 225-235.

      [31] Vladislov, V. Sidorenko, Celletti, Alessandra. (2010), A spring mass model of tethered satellites system properties of planar periodic motions, Celestial Mechanics & Dynamical Astronomy, 209-231.

      [32] Narayan, A, Pandey,M.D. (2013), Some Non-linear Parametric Resonance Oscillations Of Dumbell Satellite In Elliptical Orbit" International Journal of Applied Mathematical Research, Germany, Vol.02 No. 02, 200-212.

  • Downloads

  • How to Cite

    Narayan, A., & Pandey, M. D. (2015). Non-linear parametric resonance driven oscillations of dumbell satellite in elliptical orbit under the combined effects of magnetic field of the earth and oblateness of the earth. International Journal of Advanced Astronomy, 3(1), 1-7. https://doi.org/10.14419/ijaa.v3i1.3897