Multiple NEA rendezvous mission: Solar sailing options

  • The scientific interest in near-Earth asteroids (NEAs) and the classification of some of those as potentially hazardous asteroid for the Earth stipulated the interest in NEA exploration. Close-up observations of these objects will increase drastically our knowledge about the overall NEA population. For this reason, a multiple NEA rendezvous mission through solar sailing is investigated, taking advantage of the propellantless nature of this groundbreaking propulsion technology. Considering a spacecraft based on the DLR/ESA Gossamer technology, this work focuses on the search of possible sequences of NEA encounters. The effectiveness of this approach is demonstrated through a number of fully-optimized trajectories. The results show that it is possible to visit five NEAs within 10 years with near-term solar-sail technology. Moreover, a study on a reduced NEA database demonstrates the reliability of the approach used, showing that 58% of the sequences found with an approximated trajectory model can be converted into real solar-sail trajectories. Lastly, this second study shows the effectiveness of the proposed automatic optimization algorithm, which is able to find solutions for a large number of mission scenarios without any input required from the user.

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Metadaten
Author:Alessandro Peloni, Bernd DachwaldORCiD, Matteo Ceriotti
Parent Title (English):Fourth International Symposium on Solar Sailing
Document Type:Conference Proceeding
Language:English
Year of Completion:2017
Date of the Publication (Server):2022/06/01
Tag:Automated Optimization; Gossamer; Multiphase; Sequence-Search; Trajectory Optimization
Length:11
First Page:1
Last Page:11
Note:
Fourth International Symposium on Solar Sailing (ISSS 2017), Kyoto, Japan, 17-20 Jan 2017.
http://www.jsforum.or.jp/ISSS2017/
Link:https://eprints.gla.ac.uk/135222/1/135222.pdf
Zugriffsart:weltweit
Institutes:FH Aachen / Fachbereich Luft- und Raumfahrttechnik
FH Aachen / IfB - Institut für Bioengineering