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SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE Article Matyushin M.M., Ovechko V.M., Razoumny Y.N., Skorobogatov O.P., Tyurina D.D., Baranova I.S. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 181-188
THREE-BODY PROBLEM FOR THE EARTH-MOON SYSTEM UNDER PHOTO-GRAVITATIONAL INFLUENCE OF THE SUN Article Salnikova T., Stepanov S., Shuvalova A. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 201-208
EVALUATION OF IMPULSIVE MANEUVERS PERFORMED BY ACTIVE SPACE OBJECT Article Agapov V.M., Baranov A.A., Karatunov M.O. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 339-351
SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL BASED ON APPLICATION OF RESONANT TUNNELING DIODES IN NONLINEAR RADIO SIGNAL CONVERTERS Article Makeev M.O., Meshkov S.A., Sinyakin V.Yu., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 475-482
OPTIMIZATION OF FLYBY SCHEMES IN THE FRAMEWORK OF ADR MISSION IN LEO Article Baranov A.A., Grishko D.A. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 519-526
LOW THRUST TRANSFERS TO SPACE DEBRIS OBJECT NEIGHBORHOOD Article Budyansky A.A., Baranov A.A. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 557-565
OPTIMAL INTERPLANETARY SPACECRAFT FLIGHTS DESIGN WITH MANY-REVOLUTION BRAKING MANEUVER BY A LOW THRUST JET ENGINE Article Samokhin A.S., Samokhina M.A., Zapletin M.P., Grigoriev I.S. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 587-606
METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING Article Baranov A.A., Razoumny V.Yu., Razoumny Y.N., Malyshev V.V. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 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 Article Samokhina M.A., Samokhin A.S., Zapletin M.P., Grigoriev I.S. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 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 Article Samokhin A.S., Samokhina M.A. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 843-862
METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE Article Matyushin M.M., Razoumny Y.N., Ovechko V.M., Orlov D.A., Scorobogatov O.P., Tyurina D.D. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 863-872
CONTROL SYNTHESIS BY NETWORK OPERATOR METHOD FOR SPACECRAFT DESCENT ON THE MOON Article Diveev A.I., Sofronova E.A., Ryndin D.A. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 873-883
A MANIPULATOR ROBOT FOR FAST AND ACCURATE POSITIONING OF THE OBJECT Article Vnykov A.A., Mustary S. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 921-940
METHOD OF TETHERED SYSTEM CONTROL FOR DEORBITING OBJECTS USING EARTH'S ATMOSPHERE Article Razoumny Y.N., Kupreev S.A., Misra A.K. Advances in the Astronautical Sciences. Univelt Inc.. Vol. 161. 2017. P. 1031-1050