Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity
Crossref DOI link: https://doi.org/10.3103/S1068799818020083
Published Online: 2019-01-19
Published Print: 2018-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zubov, N. E.
Mikrin, E. A.
Ryabchenko, V. N.
Sorokin, I. V.
Text and Data Mining valid from 2018-04-01
Article History
Received: 11 April 2017
First Online: 19 January 2019