FRACTAL PYRAMID CONTROLLING ORIENTATION AND VELOCITY OF SPACECRAFT Статья Yefremov A.P. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 159-164
SPACECRAFT THRUST VECTOR CONTROL DURING LANDING ON THE MOON SURFACE Статья 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.. Том 161. 2017. С. 181-188
THREE-BODY PROBLEM FOR THE EARTH-MOON SYSTEM UNDER PHOTO-GRAVITATIONAL INFLUENCE OF THE SUN Статья Salnikova T., Stepanov S., Shuvalova A. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 201-208
EVALUATION OF IMPULSIVE MANEUVERS PERFORMED BY ACTIVE SPACE OBJECT Статья Agapov V.M., Baranov A.A., Karatunov M.O. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 339-351
SPACECRAFT GUIDANCE, NAVIGATION AND CONTROL BASED ON APPLICATION OF RESONANT TUNNELING DIODES IN NONLINEAR RADIO SIGNAL CONVERTERS Статья Makeev M.O., Meshkov S.A., Sinyakin V.Yu., Razoumny Y.N. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 475-482
OPTIMIZATION OF FLYBY SCHEMES IN THE FRAMEWORK OF ADR MISSION IN LEO Статья Baranov A.A., Grishko D.A. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 519-526
LOW THRUST TRANSFERS TO SPACE DEBRIS OBJECT NEIGHBORHOOD Статья Budyansky A.A., Baranov A.A. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 557-565
OPTIMAL INTERPLANETARY SPACECRAFT FLIGHTS DESIGN WITH MANY-REVOLUTION BRAKING MANEUVER BY A LOW THRUST JET ENGINE Статья Samokhin A.S., Samokhina M.A., Zapletin M.P., Grigoriev I.S. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 587-606
METHOD OF ENERGY ESTIMATION OF INTERORBITAL TRANSFERS FOR LEO SPACECRAFT ON-ORBIT SERVICING Статья Baranov A.A., Razoumny V.Yu., Razoumny Y.N., Malyshev V.V. Advances in the Astronautical Sciences. Univelt Inc.. 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 Статья Samokhina M.A., Samokhin A.S., Zapletin M.P., Grigoriev I.S. Advances in the Astronautical Sciences. Univelt Inc.. 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 Статья Samokhin A.S., Samokhina M.A. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 843-862
METHOD OF TWO-PARAMETERS CONTROL OF SPACECRAFT DURING DESCENT IN THE MARS ATMOSPHERE Статья 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.. Том 161. 2017. С. 863-872
CONTROL SYNTHESIS BY NETWORK OPERATOR METHOD FOR SPACECRAFT DESCENT ON THE MOON Статья Diveev A.I., Sofronova E.A., Ryndin D.A. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 873-883
A MANIPULATOR ROBOT FOR FAST AND ACCURATE POSITIONING OF THE OBJECT Статья Vnykov A.A., Mustary S. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 921-940
METHOD OF TETHERED SYSTEM CONTROL FOR DEORBITING OBJECTS USING EARTH'S ATMOSPHERE Статья Razoumny Y.N., Kupreev S.A., Misra A.K. Advances in the Astronautical Sciences. Univelt Inc.. Том 161. 2017. С. 1031-1050