Maksim Shirobokov reported about the possibility of lunar landing from near-rectilinear halo orbits. Sergey Trofimov, Maksim Shirobokov, Anastasia Tselousova, and Mikhail Ovchinnikov
Transfers Between Near-Rectilinear Halo Orbits and the Moon
[paper, presentation] Yaroslav Mashtakov presented a Lyapunov control law for the maneuver of spacecraft reorientation under constraints. Yaroslav Mashtakov, Stepan Tkachev, and Sergey Shestakov
Lyapunov Control for Attitude Maneuvers with Restricted Areas
[paper, presentation] Sergey Shestakov proposed the analytical approach to design a tetrahedral formation of low-Earth orbit satellites. Mikhail Ovchinnikov, Sergey Shestakov, and Yaroslav Mashtakov
Analytical Approach to Construction a Reference Motion for Tetrahedral Satellite Formation
[paper, presentation] Coupled attitude and relative motion control in a formation of satellites with variable-reflectivity solar sails was discussed in the presentation given by Stepan Tkachev. Yaroslav Mashtakov, Mikhail Ovchinnikov, Tatyana Petrova, and Stepan Tkachev
Attitude and Relative Motion Control of Satellites in Formation Flying via Solar Sail with Variable Reflectivity Properties
[paper, presentation] Finally, Danil Ivanov gave two talks. The former was devoted to the use of aerodynamic forces for the nanosatellite formation deployment and keeping. The latter contained the flight data analysis for the TNS-0 #2 mission. Danil Ivanov, Mikhail Mogilevsky, Uliana Monakhova, Mikhail Ovchinnikov, and Alexander Chernyshov
Deployment and Maintenance of Nanosatellite Tetrahedral Formation Using Aerodynamic Forces
[paper, presentation] Mikhail Ovchinnikov, Danil Ivanov, Oleg Pansyrnyi, Igor Fedorov, Arnold Selivanov, Oleg Khromov, Nikolay Yudanov, and Artem Sergeev
Flight Results of the Mission of TNS-0 #2 Nanosatellite Connected via Global Communication System
[paper, presentation] 
The members of our team with Prof. Hanspeter Schaub (second left)
representing the University of Colorado at Boulder
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