FRACTAL PYRAMID CONTROLLING ORIENTATION AND VELOCITY OF SPACECRAFT СтатьяYefremov A.P.Advances in the Astronautical Sciences. Том 161. 2017. С. 159-164
SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE СтатьяMatyushin 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 СтатьяSalnikova 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 СтатьяAgapov 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 СтатьяMakeev 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 СтатьяBaranov A.A., Grishko D.A.Advances in the Astronautical Sciences. Том 161. 2017. С. 519-526
LOW THRUST TRANSFERS TO SPACE DEBRIS OBJECT NEIGHBORHOOD СтатьяBudyansky 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 СтатьяSamokhin 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 СтатьяBaranov 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 СтатьяSamokhina 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 СтатьяSamokhin 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 СтатьяMatyushin 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 СтатьяDiveev 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 СтатьяVnykov 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 СтатьяRazoumny 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 СтатьяRazoumny 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 СтатьяRazoumny Y.N.Advances in the Astronautical Sciences. Том 150. 2014. С. 3117-3136