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This article is cited in 1 scientific paper (total in 1 paper)
Design, deployment and keeping of nanosatellite-based tetrahedral highly elliptical orbit formation
M. D. Koptev, S. P. Trofimov
Abstract:
The problem of designing, deploying, and keeping a highly elliptical orbit tetrahedron formation of one chief microsatellite and several deputy nanosatellites is examined. To maximize formation quality, initial orbital elements of all the satellites are searched using the K-60 supercomputing cluster. Formation deployment schemes are proposed taking into account possible orbit injection errors.
Keywords:
nanosatellite, satellite formation flying, highly elliptical orbit.
Citation:
M. D. Koptev, S. P. Trofimov, “Design, deployment and keeping of nanosatellite-based tetrahedral highly elliptical orbit formation”, Keldysh Institute preprints, 2018, 097, 28 pp.
Linking options:
https://www.mathnet.ru/eng/ipmp2457 https://www.mathnet.ru/eng/ipmp/y2018/p97
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