Statistics – Computation
Scientist
Statistics
Computation
Scientist
Faculty of Mechanics and Mathematics, Lomonosov Moscow State University
Moscow State University, Vorob'evy gory, Moscow, 119899 Russia
Conditions of the Maximum Principle in the Problem of Optimal Control over an Aggregate of Dynamic Systems and Their Application to Solution of the Problems of Optimal Control of Spacecraft Motion
Solving Optimization Problems for the Flight Trajectories of a Spacecraft with a High-Thrust Jet Engine in Pulse Formulation for an Arbitrary Gravitational Field in a Vacuum
The Fastest Maneuvers of a Spacecraft with a Jet Engine of a Large Limited Thrust in a Gravitational Field in a Vacuum
The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I
The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: II
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