A novel methodology for fast and robust computation of low-thrust orbit-raising trajectories

dc.contributor.authorSreesawet, Suwat
dc.contributor.authorDutta, Atri
dc.date.accessioned2018-07-11T20:50:01Z
dc.date.available2018-07-11T20:50:01Z
dc.date.issued2017
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractAll-electric spacecraft makes numerous revolutions during the orbit-raising to the geosynchronous equatorial orbit. This paper presents a new mathematical formulation to describe the dynamics of the spacecraft under the action of continuous thrust. Furthermore, it presents a new optimization framework that considers the proposed dynamic model to solve a sequence of optimization sub-problems for rapid and robust generation of the low-thrust orbit-raising trajectories. It is considered that the spacecraft does not thrust in the shadow of the Earth. Numerical results for different orbit-raising mission scenarios are presented to illustrate the performance of the algorithm.en_US
dc.identifier.citationSreesawet, Suwat; Dutta, Atri. 2017. A novel methodology for fast and robust computation of low-thrust orbit-raising trajectories. 27th AAS/AIAA Space Flight Mechanics, vol. 160:pp 1571-1590en_US
dc.identifier.isbn978-0-87703-637-1
dc.identifier.issn1081-6003
dc.identifier.otherWOS:000433401100095
dc.identifier.urihttp://www.univelt.com/book=6048
dc.identifier.urihttp://hdl.handle.net/10057/15370
dc.language.isoen_USen_US
dc.publisherUnivelt, Inc.en_US
dc.relation.ispartofseries27th AAS/AIAA Space Flight Mechanics;v.160
dc.subjectDesignen_US
dc.subjectTransfersen_US
dc.titleA novel methodology for fast and robust computation of low-thrust orbit-raising trajectoriesen_US
dc.typeConference paperen_US
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