Motion of a satellite with a variable mass distribution in a central field of Newtonian attraction
Russian journal of nonlinear dynamics, Tome 13 (2017) no. 4, pp. 519-531.

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Within the framework of the so-called satellite approximation, configurations of the relative equilibrium are built and their stability is analyzed. In this case the elliptic Keplerian motion of the satellite/the spacecraft tight group mass center is predefined. The attitude motion of the system does not influence its orbital motion. The principal central axes of inertia are assumed to move as a rigid body. Simultaneously masses of the body can redistribute in a way such that the values of moments of inertia can change. Thus, all configurations can perform pulsing motions changing it own dimensions. One obtains a system of equations of motion for such a compound satellite. It turns out that the resulting system of equations is similar to the well-known equation of V.V.Beletsky for the satellite in elliptic orbit planar oscillations. We use true anomaly as an independent variable as it is in the Beletsky equation. It turned out that there are planar pendulum-like librations of the whole system which may be regarded as perturbations of the mathematical pendulum. One can introduce action-angle variables in this case and can construct the dynamics of mappings over the non-autonomous perturbation period. As a result, one is able to apply the well-known Moser theorem on an invariant curve for twisting maps of annulus. After that one can get a general picture of motion in the case of the system planar oscillations. So, the whole description in the paper splits into two topics: (a) general dynamical analysis of the satellite planar attitude motion using KAM theory; (b) construction of periodic solutions families depending on the perturbation parameter and rising from equilibrium as the perturbation value grows. The latter families depend on the parameter of the perturbation and are absent in the non-perturbed problem.
Keywords: KAM theory, Moser theorem on invariant curve, periodic solutions, analytical developments.
Mots-clés : action-angle variables
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A. A. Burov; I. I. Kosenko. Motion of a satellite with a variable mass distribution in a central field of Newtonian attraction. Russian journal of nonlinear dynamics, Tome 13 (2017) no. 4, pp. 519-531. http://geodesic.mathdoc.fr/item/ND_2017_13_4_a4/

[1] Beletskii V. V., Motion of an artificial satellite about its center of mass, Israel Program for Scientific Translations, Jerusalem, 1966, x, 261 pp.

[2] Beletskii V. V., Essays on the motion of celestial bodies, Birkhäuser, Basel, 2001, 372 pp.

[3] Beletskii V. V., “On satellite libration”, Artificial Earth satellite: Vol. 3, Akad. Nauk SSSR, Moscow, 1959, 13–31 (Russian)

[4] Beletsky V. V., Giverts M. E., “Motion of a pulsating system in a gravitational field”, Kosmicheskie Issledovaniya, 5:6 (1967), 304–308 (Russian)

[5] Burov A. A., “The motion of cross-shaped bodies around a fixed point in a central Newtonian force field”, J. Appl. Math. Mech., 60:1 (1996), 25–30

[6] Burov A. A., “Oscillations of a vibrating dumbbell on an elliptic orbit”, Dokl. Phys., 56:3 (2011), 182–189

[7] Burov A. A., Karapetyan A. V., “On the motion of cross-shaped bodies”, Mech. Solids, 30:6 (1995), 11–15

[8] Burov A. A., Kosenko I. I., “Planar vibrations of a solid with variable mass distribution in an elliptic orbit”, Dokl. Phys., 56:10 (2011), 548–552

[9] Vorobyov I. I., “The peculiar travel”, Kvant, 1974, no. 2, 22–25 (Russian)

[10] Donov A. E., “Theory of a gravicraft flight”, Kosmicheskie Issledovaniya, 9:3 (1971), 393–396 (Russian)

[11] Kozlov V. V., Onishchenko D. A., “The motion in a perfect fluid of a body containing a moving point mass”, J. Appl. Math. Mech., 67:4 (2003), 553–564

[12] Kozlov V. V., Ramodanov S. M., “The motion of a variable body in an ideal fluid”, J. Appl. Math. Mech., 65:4 (2001), 579–587

[13] Kozlov V. V., Ramodanov S. M., “On the motion of a body with a rigid hull and changing geometry of masses in an ideal fluid”, Dokl. Phys., 47:2 (2002), 132–135

[14] Kosenko I. I., “Application of the theory of the Leray – Schauder degree for the approximation of oscillations of a satellite on an elliptic orbit”, Dokl. Phys., 50:10 (2005), 532–534

[15] Kosenko I. I., “The topological degree and the approximation of solutions of irregular problems in mechanics: Oscillations of a satellite in an elliptic orbit”, J. Math. Sci. (N. Y.), 149:5 (2008), 1539–1566

[16] Malkin I. G., Some problems in the theory of nonlinear oscillations: In 2 vols., United States Atomic Energy Commission, Technical Information Service, Germantown, Md., 1959, 589 pp.

[17] Markeev A. P., Libration points in celestial mechanics and space dynamics, Nauka, Moscow, 1978 (Russian)

[18] Markeev A. P., Theoretical mechanics, R Dynamics, Institute of Computer Science, Izhevsk, 2007 (Russian)

[19] Markeev A. P., Linear Hamiltonian systems and some problems of stability of the satellite center of mass, R Dynamics, Institute of Computer Science, Izhevsk, 2009 (Russian)

[20] Markov V. E., “Compensation of external perturbations applied to a spacecraft via the method of variation of its geometry of masses”, Izv. Akad. Nauk SSSR. Mekh. Tverd. Tela, 1974, no. 5, 3–9 (Russian)

[21] Moser J. K., Lectures on Hamiltonian systems, Mem. Amer. Math. Soc., 81, AMS, Providence, R.I., 1968, 60 pp.

[22] Sarychev V. A., Problems of orientation of satellites, Itogi Nauki Tekh. Ser. Issled. Kosmich. Prostr., VINITI, Moscow, 1978 (Russian)

[23] Chernous'ko F. L., “On the motion of a body containing a movable internal mass”, Dokl. Phys., 50:11 (2005), 593–597

[24] Chernous'ko F. L., “Analysis and optimization of the motion of a body controlled by means of a movable internal mass”, J. Appl. Math. Mech., 70:6 (2006), 819–842

[25] Chetaev N. G., Theoretical mechanics, Springer, Berlin, 1989, 407 pp.

[26] Amin R. A., Newton D. J., “Research into the effects of astronaut motion on the spacecraft: A review”, Acta Astronaut., 47:12 (2000), 859–869

[27] Bergamin L., Delva P., Hees A., “Vibrating systems in Schwarzschild spacetime: Towards new experiments in gravitation?”, Class. Quantum Grav., 26:18 (2009), 185006, 15 pp.

[28] Burov A. A., Chevallier D. P., “Dynamics of affinely deformable bodies from the standpoint of theoretical mechanics and differential geometry”, Rep. Math. Phys., 62:3 (2008), 283–321

[29] Burov A., Kosenko I., “On planar oscillations of a body with a variable mass distribution in an elliptic orbit”, Proc. Inst. Mech. Eng. C J. Mech. Eng. Sci., 225:10 (2011), 2288–2295

[30] Burov A., Kosenko I., “On planar oscillations of a body with a variable mass distribution in an elliptic orbit”, Proc. of the 7th European Nonlinear Dynamics Conference (ENOC'2011), eds. D. Bernardini, G. Rega, F. Romeo, Univ. di Roma, Sapienza, 2011

[31] Gratus J., Tucker R., “An improved method of gravicraft propulsion”, Acta Astronaut., 53:3 (2003), 161–172

[32] Iñarrea M., Lanchares V., “Chaos in the reorientation process of a dual-spin spacecraft with time-dependent moments of inertia”, Internat. J. Bifur. Chaos Appl. Sci. Engrg., 10:5 (2000), 997–1018

[33] Iñarrea M., Lanchares V., “Chaotic pitch motion of an asymmetric non-rigid spacecraft with viscous drag in circular orbit”, Internat. J. Non-Linear Mech., 41:1 (2006), 86–100

[34] Iñarrea M., Lanchares V., Rothos V. M., Salas J. P., “Chaotic rotations of an asymmetric body with time-dependent moments of inertia and viscous drag”, Internat. J. Bifur. Chaos Appl. Sci. Engrg., 13:2 (2003), 393–409

[35] Landis G., “Reactionless orbital propulsion using tether deployment”, Acta Astronaut., 26:5 (1992), 307–312

[36] Levi-Civita T., “Sur la résolution qualitative du problème restreinte des trois corps”, Acta Math., 30:1 (1906), 305–327

[37] Longo M. J., “Swimming in Newtonian space-time: Orbital changes by cyclic changes in body shape”, Am. J. Phys., 72:10 (2004), 1312–1315

[38] Nechvile V., “Sur une forme nouvelle d'équations différentielles du problème restreint elliptique”, C. R. Acad. Sci. Paris, 182 (1926), 310–311

[39] Pascal M., “Sur le mouvement d'un triple bâtonnet dans un champ Newtonien”, J. Méc., 11:1 (1972), 147–160

[40] Schaefer J. F., “Artificial satellite orbit shifting without mass expulsion utilizing gravity gradient”, Proc. of the 17th Internat. Astronautical Congr. (Madrid, Spain, Oct 1966), 9 pp.

[41] Thomson W. T., Fung Y. C., “Instability of spinning space stations due to crew motion”, AIAA J., 3:6 (1965), 1082–1087

[42] Wisdom J., “Swimming in spacetime: Motion by cyclic changes in body shape”, Science, 299 (2003), 1865–1869