Geodesic
Determination of trajectory parameters of small satellite motion using its primary measurements
Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 1 (2016), pp. 64-68 
A. A. Golovan; A. Dzhepe. Determination of trajectory parameters of small satellite motion using its primary measurements. Vestnik Moskovskogo universiteta. Matematika, mehanika, no. 1 (2016), pp. 64-68. http://geodesic.mathdoc.fr/item/VMUMM_2016_1_a12/
@article{VMUMM_2016_1_a12,
     author = {A. A. Golovan and A. Dzhepe},
     title = {Determination of trajectory parameters of small satellite motion using its primary measurements},
     journal = {Vestnik Moskovskogo universiteta. Matematika, mehanika},
     pages = {64--68},
     year = {2016},
     number = {1},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/VMUMM_2016_1_a12/}
}
TY  - JOUR
AU  - A. A. Golovan
AU  - A. Dzhepe
TI  - Determination of trajectory parameters of small satellite motion using its primary measurements
JO  - Vestnik Moskovskogo universiteta. Matematika, mehanika
PY  - 2016
SP  - 64
EP  - 68
IS  - 1
UR  - http://geodesic.mathdoc.fr/item/VMUMM_2016_1_a12/
LA  - ru
ID  - VMUMM_2016_1_a12
ER  - 
%0 Journal Article
%A A. A. Golovan
%A A. Dzhepe
%T Determination of trajectory parameters of small satellite motion using its primary measurements
%J Vestnik Moskovskogo universiteta. Matematika, mehanika
%D 2016
%P 64-68
%N 1
%U http://geodesic.mathdoc.fr/item/VMUMM_2016_1_a12/
%G ru
%F VMUMM_2016_1_a12

Voir la notice de l'article provenant de la source Math-Net.Ru

The problem of determining the motion parameters of a small satellite on the basis of satellite navigation equipment is studied. A raw data processing algorithm is proposed when the satellite measurements are not always regular.

[1] Golovan A.A., Parusnikov N.A., Matematicheskie osnovy navigatsionnykh sistem, v. I, Matematicheskie modeli inertsialnoi navigatsii, 3-e izd., ispravlennoe i dopolnennoe, MAKS Press, M., 2011

[2] Golovan A.A., Parusnikov N.A., Matematicheskie osnovy navigatsionnykh sistem, v. II, Prilozheniya metodov optimalnogo otsenivaniya k zadacham navigatsii, 2-e izd., ispravlennoe i dopolnennoe, MAKS Press, M., 2012

[3] Vavilova N.B., Golovan A.A., Parusnikov N.A., Trubnikov S.A., Matematicheskie modeli i algoritmy obrabotki izmerenii sputnikovoi navigatsionnoi sistemy GPS. Standartnyi rezhim, Izd-vo MGU, M., 2009

[4] Globalnaya sputnikovaya navigatsionnaya sistema GLONASS, Interfeisnyi kontrolnyi dokument GLONASS (redaktsiya 5.1), M., 2008 http://www.spacecorp.ru

[5] Aleksandrov V.V., Belenkii A.D., Bugrov D.I., Lebedev A.V., Lemak S.S., Gerrero Sanchez V.F., “Otsenka tochnosti orientatsii po telemetrii sputnika “Tatyana-2””, Vestn. Mosk. un-ta. Matem. Mekhan., 2011, no. 3, 69–72