METHOD OF TETHERED SYSTEM CONTROL FOR DEORBITING OBJECTS USING EARTH'S ATMOSPHERE ArticleRazoumny Y.N., Kupreev S.A., Misra A.K.Advances in the Astronautical Sciences. Том 161. 2017. С. 1031-1050
GROUND SPACECRAFT CONTROL FACILITIES DISTRIBUTION BY METHOD OF SUCCESSIVE ELIMINATION OF CONFLICTING SITUATIONS ArticleMatyushin M.M., Ovechko V.M., Polivnikov V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D.Advances in the Astronautical Sciences. Том 161. 2017. С. 1065-1075
OPTIMAL FORMATION AND REPLENISHMENT OF LUNAR SATELLITE CONSTELLATIONS ArticleBaranov A.A., Grishko D.A., Vasilkov B.O.Advances in the Astronautical Sciences. Том 161. 2017. С. 1087-1095
THE MAINTENANCE OF A GIVEN CONFIGURATION OF A SYSTEM OF TWO SATELLITES ArticleChernov N.V., Vikhrachev V.O.Advances in the Astronautical Sciences. Том 161. 2017. С. 1141-1147
ON OPTIMIZATION OF TWO-TIER WALKER DELTA PATTERNS SATELLITE CONSTELLATIONS TO PROVIDE CONTINUOUS COVERAGE OF NEAR-EARTH SPACE SPHERICAL LAYER ArticleRazoumny Y.N., Samusenko O.E., Quy N.N.Advances in the Astronautical Sciences. Том 161. 2017. С. 1149-1159
FRACTAL PYRAMID CONTROLLING ORIENTATION AND VELOCITY OF SPACECRAFT ArticleYefremov A.P.Advances in the Astronautical Sciences. Том 161. 2017. С. 159-164
SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE ArticleMatyushin M.M., Ovechko V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D., Baranova I.S.Advances in the Astronautical Sciences. Том 161. 2017. С. 181-188
THREE-BODY PROBLEM FOR THE EARTH-MOON SYSTEM UNDER PHOTO-GRAVITATIONAL INFLUENCE OF THE SUN ArticleSalnikova T., Stepanov S., Shuvalova A.Advances in the Astronautical Sciences. Том 161. 2017. С. 201-208
EVALUATION OF IMPULSIVE MANEUVERS PERFORMED BY ACTIVE SPACE OBJECT ArticleAgapov V.M., Baranov A.A., Karatunov M.O.Advances in the Astronautical Sciences. Том 161. 2017. С. 339-351
SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL BASED ON APPLICATION OF RESONANT TUNNELING DIODES IN NONLINEAR RADIO SIGNAL CONVERTERS ArticleMakeev M.O., Meshkov S.A., Sinyakin V.Yu., Razoumny Y.N.Advances in the Astronautical Sciences. Том 161. 2017. С. 475-482
OPTIMIZATION OF FLYBY SCHEMES IN THE FRAMEWORK OF ADR MISSION IN LEO ArticleBaranov A.A., Grishko D.A.Advances in the Astronautical Sciences. Том 161. 2017. С. 519-526
LOW THRUST TRANSFERS TO SPACE DEBRIS OBJECT NEIGHBORHOOD ArticleBudyansky A.A., Baranov A.A.Advances in the Astronautical Sciences. Том 161. 2017. С. 557-565
OPTIMAL INTERPLANETARY SPACECRAFT FLIGHTS DESIGN WITH MANY-REVOLUTION BRAKING MANEUVER BY A LOW THRUST JET ENGINE ArticleSamokhin A.S., Samokhina M.A., Zapletin M.P., Grigoriev I.S.Advances in the Astronautical Sciences. Том 161. 2017. С. 587-606
METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING ArticleBaranov A.A., Razoumny V.Yu., Razoumny Y.N., Malyshev V.V.Advances in the Astronautical Sciences. Том 161. 2017. С. 701-709
METHOD OF OPTIMAL TRAJECTORIES DESIGN FOR A SPACECRAFT WITH A JET ENGINE OF A LARGE LIMITED THRUST IN PROBLEMS WITH THE PHASING CONDITION ArticleSamokhina M.A., Samokhin A.S., Zapletin M.P., Grigoriev I.S.Advances in the Astronautical Sciences. Том 161. 2017. С. 711-730