The almost constant-speed two-body problem with resistance

Mavraganis, AG

dc.contributor.author	Mavraganis, AG	en
dc.date.accessioned	2014-03-01T01:08:34Z
dc.date.available	2014-03-01T01:08:34Z
dc.date.issued	1991	en
dc.identifier.issn	0923-2958	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/10577
dc.subject	Artificial satellite	en
dc.subject	drag effect	en
dc.subject.classification	Astronomy & Astrophysics	en
dc.subject.classification	Mathematics, Interdisciplinary Applications	en
dc.title	The almost constant-speed two-body problem with resistance	en
heal.type	journalArticle	en
heal.identifier.primary	10.1007/BF00052930	en
heal.identifier.secondary	http://dx.doi.org/10.1007/BF00052930	en
heal.language	English	en
heal.publicationDate	1991	en
heal.abstract	The almost constant-speed motion of a mass acted upon by a Newtonian attraction and a resisting force is treated. The equation of orbit is derived for a specific type of resistance which covers the familiar case of Danby's drag(=αr-2) whilst the vector invariants are obtained by direct operation on the vector form of the equation of motion. © 1991 Kluwer Academic Publishers.	en
heal.publisher	Kluwer Academic Publishers	en
heal.journalName	Celestial Mechanics and Dynamical Astronomy	en
dc.identifier.doi	10.1007/BF00052930	en
dc.identifier.isi	ISI:000207116000007	en
dc.identifier.volume	51	en
dc.identifier.issue	4	en
dc.identifier.spage	395	en
dc.identifier.epage	405	en