Physics
Scientist
Research Institute of Applied Mathematics and Electrodynamics
Khrunichev State Center of Space Research and Production, Novozavodskaya 18, Moscow, Russia
Khrunichev State Research and Production Space Center
Evolution of orbits in the twice-averaged Hill problem under the effect of a small transverse acceleration.
Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit
Optimization of interplanetary trajectories for spacecraft with ideally regulated engines using the continuation method
Optimization of Multi-Orbit Transfers between Noncoplanar Elliptic Orbits
Quasioptimal control with feedback for multiorbit low-thrust transfer between noncoplanar elliptic and circular orbits
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