Please use this identifier to cite or link to this item:
http://hdl.handle.net/2248/1585
Full metadata record
DC Field | Value | Language |
---|---|---|
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 |
Appears in Collections: | BASI Publications |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
Paper_4.pdf | 546.42 kB | Adobe PDF | ![]() View/Open |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.