Non-linear planar oscillation of a satellite in elliptical orbit under the influence of solar radiation pressure, 1

dc.contributor.author	Bhatnagar, K. B
dc.contributor.author	Khan, A
dc.contributor.author	Saha, L. M
dc.date.accessioned	2007-05-11T11:37:32Z
dc.date.available	2007-05-11T11:37:32Z
dc.date.issued	1994
dc.identifier.citation	BASI, Vol. 22, No. 1, pp. 47-58	en
dc.identifier.uri	http://hdl.handle.net/2248/1585
dc.description.abstract	The non-linear oscillations of a satellite in an elliptic orbit around the earth under the influence of the solar radiation pressure have been studied in a series of papers 1 and 2. In paper 1, by using Melnikov's method the equations of motion have been shown to be non-integrable. The radiation pressure has been taken of the order of eccentricity e (e much less than 1) and therefore the solution is obtained by using BKM method in non-resonance case. It is observed that the amplitude of the oscillation remains constant up to second approximation. In paper 2, we have studied the resonance case and the chaotic nature of the given dynamical system	en
dc.format.extent	559539 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en	en
dc.publisher	Astronomical Society of India	en
dc.subject	Celestial mechanics	en
dc.subject	solar system	en
dc.title	Non-linear planar oscillation of a satellite in elliptical orbit under the influence of solar radiation pressure, 1	en
dc.type	Article	en