Evasive Maneuvers in Space Debris Environment and Technological Parameters

dc.contributorUniversidade Estadual Paulista (UNESP)
dc.creatorJesus, Antonio D. C.
dc.creatorRibeiro, Rafael S.
dc.creatorRossi, Alessandro
dc.creatorVeira Neto, Ernesto
dc.date2014-05-20T13:28:06Z
dc.date2014-05-20T13:28:06Z
dc.date2012-01-01
dc.date.accessioned2017-04-05T20:10:21Z
dc.date.available2017-04-05T20:10:21Z
dc.identifierMathematical Problems In Engineering. New York: Hindawi Publishing Corporation, p. 15, 2012.
dc.identifier1024-123X
dc.identifierhttp://hdl.handle.net/11449/9312
dc.identifier10.1155/2012/126521
dc.identifierWOS:000310635600001
dc.identifierWOS000310635600001.pdf
dc.identifierhttp://dx.doi.org/10.1155/2012/126521
dc.identifier.urihttp://repositorioslatinoamericanos.uchile.cl/handle/2250/857491
dc.descriptionWe present a study of collisional dynamics between space debris and an operational vehicle in LEO. We adopted an approach based on the relative dynamics between the objects on a collisional course and with a short warning time and established a semianalytical solution for the final trajectories of these objects. Our results show that there are angular ranges in 3D, in addition to the initial conditions, that favor the collisions. These results allowed the investigation of a range of technological parameters for the spacecraft (e.g., fuel reserve) that allow a safe evasive maneuver (e.g., time available for the maneuver). The numerical model was tested for different values of the impact velocity and relative distance between the approaching objects.
dc.descriptionConselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)
dc.descriptionFundação de Amparo à Pesquisa do Estado de São Paulo (FAPESP)
dc.languageeng
dc.publisherHindawi Publishing Corporation
dc.relationMathematical Problems in Engineering
dc.rightsinfo:eu-repo/semantics/openAccess
dc.titleEvasive Maneuvers in Space Debris Environment and Technological Parameters
dc.typeOtro


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