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