1Department of Mathematics, School of Basic and Applied Sciences Guru Gobind Singh Indraprastha University, Kashmere Gate, Delhi-110 006, India
*Author for Correspondence, E-mail: rashmi@ipu.edu; rb_22@rediffmail.com
This paper deals with the study of the non-linear planar oscillation of a satellite in a circular orbit under the influence of aerodynamic torque. Throught Melnikov's method, we have discussed that the equations of motion are non-integrable. The non-integrability in Earth-Satellite system has also been discussed graphically.
70M, 74G25, Aerodynamic torque, Air drag, Non-linear, Planar oscillation