Geodesic
Aerodynamic Torque exhibits non –resonance oscillation in satellite motion
Mathematica Applicanda, Tome 44 (2016) no. 2, pp. 247-262 Cet article a éte moissonné depuis la source Annales Societatis Mathematicae Polonae Series

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This paper deals with the non-linear oscillation of a satellite in an elliptic orbit around the Earth under the influence of aerodynamic and gravitational torque. It is assumed that the orbital plane coincides with the equatorial plane of the Earth. Using Bogoliubov- Krylov- Mitropolsky (BKM) methods of nonlinear oscillations, it is observed that the amplitude of the oscillation remains constant up to the second order of approximation. Numerically time series, 2D and 3D phase spaces are plotted for Earth Moon system using Matlab. The existence of main and parametric resonance concludes the different frequency states which transit the motion from regular to chaotic state.
DOI : 10.14708/ma.v44i2.1217
Classification : 70K42
Mots-clés : Aerodynamic torque, Gravitational torque, Non-linear oscillation, Non-Resonance, Resonance 
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Rashmi Bhardwaj; Manjeet Kaur. Aerodynamic Torque exhibits non –resonance oscillation in satellite motion. Mathematica Applicanda, Tome 44 (2016) no. 2, pp.  247-262. doi: 10.14708/ma.v44i2.1217

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