Application of the Local Estimation Methods to Calculate the Radiant Intensity of a High-Temperature Jet von Grigoriev, I. S.

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Inserting a Maximum-Mass Spacecraft into a Target Orbit Using a Limited-Thrust Engine with Releasing the Separable Part of Its Launch Vehicle into the Earth’s Atmosphere von Grigoriev, I. S., Proskuryakov, A. I.

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Spacecraft Transfer Optimization with Releasing the Additional Fuel Tank and the Booster to the Earth Atmosphere von Grigoriev, I. S., Proskuryakov, A. I.

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Research on the development of the agricultural sector of the Northern zone: repair and maintenance of machines von Kokieva, G E, Druzyanova, V P, Grigoriev, S I

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Thermal Conductivity of Phase Changing Materials Doped with Carbon Nanotubes von Bocharov, G S, Gerasimov, D N, Grigoriev, I S, Dedov, A V, Zverev, M A, Eletskii, A V

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Optimizing Flight Trajectories for Space Vehicles with an Additional Fuel Tank. II von Grigoriev, I. S., Danilina, I. A.

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A Thermal Accumulator Based on Phase-Change Materials von Bocharov, G. S., Vagin, A. O., Grigoriev, I. S., Dedov, A. V., Eletskii, A. V., Zakharenkov, A. V., Zverev, M. A.

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Optimizing flight trajectories for space vehicles with an additional fuel tank. I von Grigoriev, I. S., Danilina, I. A.

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New age datings of gabbroides of the Kershor complex (Polar Urals) von Remizov, D. N., Grigoriev, S. I., Petrov, S. Yu, Kos’yanov, A. O., Nosikov, M. V., Sergeev, S. A.

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Multilevel Governance and Resource Exchange: Votes, Budgets, Information von Grigoriev, IS, Dekalchuk, AA, Gubaydullina, SSh

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Inserting a Maximum-Mass Spacecraft into a Target Orbit Using a Limited-Thrust Engine with Releasing the Separable Part of Its Launch Vehicle into the Earth’s Atmosphere von Grigoriev, I. S., Proskuryakov, A. I.

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Inserting a Maximum-Mass Spacecraft into a Target Orbit Using a Limited-Thrust Engine with Releasing the Separable Part of Its Launch Vehicle into the Earth’s Atmosphere von Grigoriev, I. S, Proskuryakov, A. I

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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 S... von Grigoriev, I S, Grigoriev, K G

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One optimization problem for trajectories of spacecraft rendezvous mission to a group of asteroids von Grigoriev, I. S., Zapletin, M. P.

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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 limi... von Grigoriev, I. S., Grigoriev, K. G.

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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 von Grigoriev, I S, Grigoriev, K G

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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 limi... von Grigoriev, I. S., Grigoriev, K. G.

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First ACT global trajectory optimisation competition: Results found at Moscow State University von Grigoriev, I.S., Zapletin, M.P., Zapletina, E.V.

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About one problem of trajectory optimization von Grigoriev, I. S., Zapletin, M. P.

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On solving the problems of optimization of trajectories of many-revolution orbit transfers of spacecraft von Ryzhov, S. Yu, Grigoriev, I. S.

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