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KIAM Preprint  97, Moscow, 2018
Authors: Koptev M.D., Trofimov S.P.
Design, deployment and keeping of nanosatellite-based tetrahedral highly elliptical orbit formation
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.
nanosatellite, satellite formation flying, highly elliptical orbit
Publication language: russian,  pages: 28
Research direction:
Theoretical and applied problems of mechanics
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About authors:
  • Koptev Mikhail Dmitriyevich,
  • Trofimov Sergey Pavlovich, RAS