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Application of asteroid redirection methods to orbital debris removal
Institute for Aerospace Studies, University of Toronto.
Luleå tekniska universitet, Institutionen för system- och rymdteknik, Rymdteknik.
Rekke forfattare: 2
2016 (engelsk)Inngår i: 2016 IEEE Aerospace Conference: AERO 2016, Big Sky, United States, 5 - 12 March 2016, Piscataway, NJ: IEEE Communications Society, 2016, 7500750Konferansepaper, Publicerat paper (Fagfellevurdert)
Abstract [en]

This paper discusses the applicability of some of the asteroid redirection methods, prominently studied in the literature, to orbital debris removal. The tasks of asteroid redirection and orbital debris removal share the common goal of controlled redirection of an uncooperative target. Three asteroid redirection methods are systematically compared and analyzed to assess their viability for an orbital debris reentry mission, i.e., ion beam shepherd, laser sublimation, and tugboat. These methods are investigated in terms of the characteristics of the orbital debris population and based on the major criteria for mission design of controlled reentry of uncooperative objects. In addition, the uncertainty intrinsic to the orbital debris population is quantified through the use of a Monte Carlo simulation, which provides insight into the robustness of the methods for various ranges of orbital debris. The Analytical Hierarchy Process will be employed to assess the viability of each method in a logically consistent fashion, namely, through aggregation of the relative preference (of each method) and relative importance (of each criterion). The advantages and drawbacks of each redirection method are discussed in light of the assessment results for orbital debris reentry

sted, utgiver, år, opplag, sider
Piscataway, NJ: IEEE Communications Society, 2016. 7500750
Serie
I E E E Aerospace Conference. Proceedings, ISSN 1095-323X
HSV kategori
Forskningsprogram
Rymdtekniska system
Identifikatorer
URN: urn:nbn:se:ltu:diva-30650DOI: 10.1109/AERO.2016.7500750ISI: 000388374902066Lokal ID: 48614a44-c4dd-42b8-ab8a-905c0b7b13e4ISBN: 9781467376761 (digital)OAI: oai:DiVA.org:ltu-30650DiVA: diva2:1003879
Konferanse
IEEE Aerospace Conference : 05/03/2016 - 12/03/2016
Merknad

Godkänd; 2016; 20160816 (andbra)

Tilgjengelig fra: 2016-09-30 Laget: 2016-09-30 Sist oppdatert: 2017-10-20bibliografisk kontrollert

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