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dc.contributor.authorDu, Bingxiao
dc.contributor.authorZhao, Yong
dc.contributor.authorDutta, Atri
dc.contributor.authorYu, Jing
dc.contributor.authorChen, Xiaoqian
dc.date.accessioned2015-06-25T18:31:22Z
dc.date.available2015-06-25T18:31:22Z
dc.date.issued2015-06-15
dc.identifier.citationDu, Bingxiao; Zhao, Yong; Dutta, Atri; Yu, Jing; Chen, Xiaoqian. 2015. Optimal scheduling of multispacecraft refueling based on cooperative maneuver. Advances in Space Research, vol. 55:no. 12, 15 June 2015:pp 2808–2819en_US
dc.identifier.issn0273-1177
dc.identifier.otherWOS:000355367600002
dc.identifier.urihttp://dx.doi.org/10.1016/j.asr.2015.02.025
dc.identifier.urihttp://hdl.handle.net/10057/11301
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractThe scheduling of multispacecraft refueling based on cooperative maneuver in a circular orbit is studied in this paper. In the proposed scheme, both of the single service vehicle (SSV) and the target satellite (TS) perform the orbital transfer to complete the rendezvous at the service places. When a TS is refueled by the SSV, it returns to its original working slot to continue its normal function. In this way, the SSV refuels the TS one by one. A MINLP model for the mission is first built, then a two-level hybrid optimization approach is proposed for determining the strategy, and the optimal solution is successfully obtained by using an algorithm which is a combination of Multi-island Genetic Algorithm and Sequential Quadratic Programming. Results show the cooperative strategy can save around 27.31% in fuel, compared with the non-cooperative strategy in which only the SSV would maneuver in the-example considered. Three conclusions can be drawn based on the numerical simulations for the evenly distributed constellations. Firstly, in the cooperative strategy one of the service positions is the initial location of the SSV, other service positions are also target slots, i.e. not all targets need to maneuver, and there may be more than one TS serviced in a given service position. Secondly, the efficiency gains for the cooperative strategy are higher for larger transferred fuel mass. Thirdly, the cooperative strategy is less efficient for targets with larger spacecraft mass.en_US
dc.description.sponsorshipNational Natural Science Foundation of China under Grant Nos. 91216201 and 51205403.en_US
dc.language.isoen_USen_US
dc.publisherElsevier B.V.en_US
dc.relation.ispartofseriesAdvances in Space Research;v.55:no.12
dc.subjectCooperative maneuveren_US
dc.subjectRefueling strategyen_US
dc.subjectMultispacecraften_US
dc.subjectMulti-island Genetic Algorithmen_US
dc.subjectOptimizationen_US
dc.titleOptimal scheduling of multispacecraft refueling based on cooperative maneuveren_US
dc.typeArticleen_US
dc.rights.holder(C) 2015 COSPAR. Published by Elsevier Ltd. All rights reserved.


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  • AE Research Publications [101]
    Research publications authored by the Department of Aerospace Engineering faculty and graduate students.

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