%0 Journal Article
%A E. A. Kozlov
%A Yu. N. Chelnokov
%A I. A. Pankratov
%T Investigation of the problem of optimal correction of angular elements of the spacecraft orbit using quaternion differential equation of orbit orientation
%J Izvestiya of Saratov University. Mathematics. Mechanics. Informatics
%D 2016
%P 336-344
%V 16
%N 3
%I mathdoc
%U http://geodesic.mathdoc.fr/item/ISU_2016_16_3_a11/
%G ru
%F ISU_2016_16_3_a11