INVESTIGATING THE EFFECTS OF AN OBLATE SATELLITE ON EQUILIBRIUMPOINTS FOR PHOTOGRAVITATIONAL ELLIPTIC RESTRICTED THREE-BODY PROBLEM (ER3BP)

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dc.contributor.authorSA’AD, Maryam
dc.date.accessioned2021-06-08T09:40:04Z
dc.date.available2021-06-08T09:40:04Z
dc.date.issued2019-12
dc.descriptionA DISSERTATION SUBMITTED TO THE SCHOOL OF POSTGRADUATESTUDIES AHMADU BELLO UNIVERSITY IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE AWARD OF MASTER OF SCIENCE DEGREE IN MATHMEATICS DEPARTMENT OF MATHEMATICS, FACUTLY OF PHYSICAL SCIENCES, AHMADU BELLO UNIVERSITY, ZARIA, NIGERIAen_US
dc.description.abstractWe investigate in the elliptic framework of the restricted problem of three-bodies, the motion of an oblate infinitesimal particle in the vicinity of a luminous primary and an oblate secondary. The locations and stability of the equilibrium points are found to be affected by the eccentricity, oblatenessand radiation pressure parameters. We highlights the effects of the said parameters on the locations of the triangular points and stabilityusing CEN X-3 model. The triangular points are also found to be stable for 0    C ; where  is the mass ratio  1  2   . Further analysis indicates that collinear points remain unstable in spite of the introduction of these parameters.en_US
dc.identifier.urihttp://hdl.handle.net/123456789/12423
dc.language.isoenen_US
dc.subjectINVESTIGATING,en_US
dc.subjectEFFECTS OF AN OBLATE SATELLITE,en_US
dc.subjectEQUILIBRIUMPOINTS,en_US
dc.subjectHOTOGRAVITATIONAL ELLIPTIC RESTRICTED,en_US
dc.subjectTHREE-BODY PROBLEMen_US
dc.titleINVESTIGATING THE EFFECTS OF AN OBLATE SATELLITE ON EQUILIBRIUMPOINTS FOR PHOTOGRAVITATIONAL ELLIPTIC RESTRICTED THREE-BODY PROBLEM (ER3BP)en_US
dc.typeThesisen_US
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