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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
VERIFICATION OF THE SECOND-ORDER OPTIMALITY CONDITIONS IN THE MODELING OF THE SC EXPEDITION WITH THE RETURNING TO THE EARTH BASED ON TWO LAMBERT'S PROBLEMS SOLVING ArticleSamokhin A.S., Samokhina M.A.Advances in the Astronautical Sciences. Том 161. 2017. С. 843-862
METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE ArticleMatyushin M.M., Razoumny Y.N., Ovechko V.M., Orlov D.A., Scorobogatov O.P., Tyurina D.D.Advances in the Astronautical Sciences. Том 161. 2017. С. 863-872
CONTROL SYNTHESIS BY NETWORK OPERATOR METHOD FOR SPACECRAFT DESCENT ON THE MOON ArticleDiveev A.I., Sofronova E.A., Ryndin D.A.Advances in the Astronautical Sciences. Том 161. 2017. С. 873-883
A MANIPULATOR ROBOT FOR FAST AND ACCURATE POSITIONING OF THE OBJECT ArticleVnykov A.A., Mustary S.Advances in the Astronautical Sciences. Том 161. 2017. С. 921-940
EMULATING OF THE STATIONARY OBSERVATION OF THE EARTH LOCAL REGION USING LOCALLY GEOSTATIONARY ELLIPTIC ORBITS ArticleRazoumny Y.N.Advances in the Astronautical Sciences. Том 158. 2016. С. 2933-2943
METHOD FOR CONSTELLATION DESIGN FOR EARTH PERIODIC COVERAGE USING COMPOUND SATELLITE STRUCTURES ON ORBITS WITH SYNCHRONIZED NODAL REGRESSION ArticleRazoumny Y.N.Advances in the Astronautical Sciences. Том 158. 2016. С. 2965-2979
NEW RESEARCH METHODOLOGY FOR EARTH PERIODIC COVERAGE AND REGULARITIES IN PARAMETRIC LOCALIZATION OF OPTIMAL LOW-EARTH-ORBIT SATELLITE CONSTELLATIONS ArticleRazoumny Y.N.Advances in the Astronautical Sciences. Том 150. 2014. С. 3117-3136