IJPAM: Volume 72, No. 2 (2011)
DUMBELL SATELLITE IN ELLIPTICAL ORBIT


Department of Mathematics
Bhilai Institute of Technology
Bhilai House, Durg, India
Abstract. Condition of Non-linear stability of dumbell satellites, in
elliptical orbit in the central gravitational field of force under
the combined effects of various perturbing forces has been studied.
The system comprises of two satellites connected by a light, flexible
and inextensible cable, moves with tight cable like a dumbell satellite
in elliptical orbit, in the central gravitational field of force. The gravitational field of the Earth is the main force governing the
motion and various perturbing forces like magnetic field of the Earth,
oblateness of the Earth and forces of general nature are considered
to be perturbing forces, disturbing in nature. Non-linear oscillations
of dumbell satellites about the equilibrium position in the neighbourhood
of main resonance , under the influence of perturbing
forces which is suitable for exploiting the method of Bogoliubov-Krilov
and Mitropoloskey, has been discussed, considering 'e' to be samll
parameter and the condition of stability of dumbell satellites has
been discussed using poicare method. It has been observed that the
discontinuing in the amplitude of oscillations occur at a frequency
less than the natural frequency.This discontinuity of amplitude of
oscillations of the system is important for analysing the condition
of stability of dumbell satellite in elliptical orbit.
Received: July 6, 2011
AMS Subject Classification: 70F15
Key Words and Phrases: condition of stability, perturbing forces, dynamical system, non-linear oscillation
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Source: International Journal of Pure and Applied Mathematics
ISSN printed version: 1311-8080
ISSN on-line version: 1314-3395
Year: 2011
Volume: 72
Issue: 2