Adaptive Methods of the Flybys Constructing in the Jovian System with the Orbiter Insertion Around the Galilean Moon     

Golubev  Yu. F.  Grushevskii  A. V.  Koryanov  V. V.  Lavrenov  S. M.  Tuchin  A. G.  Tuchin  D. A. 《Solar System Research》2020,54(4):318-328

Solar System Research - We consider space expeditions with a long-term spacecraft stay near the studied celestial body (artificial satellites of small bodies of the Solar System), or expeditions...  相似文献   

Main methods of trajectory synthesis for scenarios of space missions with gravity assist maneuvers in the system of Jupiter and with landing on one of its satellites     

Golubev  Yu. F.  Tuchin  A. G.  Grushevskii  A. V.  Koryanov  V. V.  Tuchin  D. A.  Morskoy  I. M.  Simonov  A. V.  Dobrovolskii  V. S. 《Solar System Research》2016,50(7):597-603

The development of a methodology for designing trajectories of spacecraft intended for the contact and remote studies of Jupiter and its natural satellites is considered. This methodology should take into account a number of specific features. Firstly, in order to maintain the propellant consumption at an acceptable level, the flight profile, ensuring the injection of the spacecraft into orbit around the Jovian moon, should include a large number of gravity assist maneuvers both in the interplanetary phase of the Earth-to-Jupiter flight and during the flight in the system of the giant planet. Secondly, the presence of Jupiter’s powerful radiation belts also imposes fairly strict limitations on the trajectory parameters.

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Analysis of Optimal Flight Trajectories to the Trans-Neptunian Object (90377) Sedna     

Zubko  V. A.  Sukhanov  A. A.  Fedyaev  K. S.  Koryanov  V. V.  Belyaev  A. A. 《Astronomy Letters》2021,47(3):188-195

Astronomy Letters - We present the results of our analysis of the optimal flight to the trans-Neptunian object (90377) Sedna at the launch in 2029. Sedna is a distant space object with a perihelion...  相似文献   

Main Property of the Jacobi Integral for Gravity Assist Maneuvers in the Solar System     

Golubev  Yu. F.  Grushevskii  A. V.  Kiseleva  I. P.  Koryanov  V. V.  Tuchin  A. G.  Tuchin  D. A. 《Solar System Research》2019,53(6):473-480

Solar System Research - In the context of the circular restricted three-body problem (RTBP), the search for the spacecraft’s asymptotic velocity $${{V}_{\infty }}$$ for gravity assist...  相似文献