An approach to forming the design performance of the attitude control system for small spacecraft
Crossref DOI link: https://doi.org/10.3103/S1068799815040030
Published Online: 2016-04-05
Published Print: 2015-10
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Alifanov, O. M.
Egorov, Yu. G.
Kul’kov, V. M.
Terent’ev, V. V.
Firsyuk, S. O.
Text and Data Mining valid from 2015-10-01