PROCYON Mission Reanalysis: Low-Thrust Asteroid Flyby Trajectory Design leveraging Convex Programming
Crossref DOI link: https://doi.org/10.1007/s40295-021-00299-4
Published Online: 2022-02-04
Published Print: 2022-02
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Ozaki, Naoya http://orcid.org/0000-0002-8445-1575
Oguri, Kenshiro
Funase, Ryu
Funding for this research was provided by:
Japan Society for the Promotion of Science (19K15214)
Masason Foundation
Text and Data Mining valid from 2022-02-01
Version of Record valid from 2022-02-01
Article History
Accepted: 9 December 2021
First Online: 4 February 2022