TY  - JOUR
AU  - E. A. Kozlov
AU  - Yu. N. Chelnokov
AU  - I. A. Pankratov
TI  - Investigation of the problem of optimal correction of angular elements of the spacecraft orbit using quaternion differential equation of orbit orientation
JO  - Izvestiya of Saratov University. Mathematics. Mechanics. Informatics
PY  - 2016
SP  - 336
EP  - 344
VL  - 16
IS  - 3
PB  - mathdoc
UR  - http://geodesic.mathdoc.fr/item/ISU_2016_16_3_a11/
LA  - ru
ID  - ISU_2016_16_3_a11
ER  -