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Application of the Local Estimation Methods to Calculate the Radiant Intensity of a High-Temperature Jet

High temperature, 2022-10, Vol.60 (5), p.688-698

Grigoriev, I. S.

2022

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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

Automation and remote control, 2024, Vol.85 (1), p.14-32

2024

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Spacecraft Transfer Optimization with Releasing the Additional Fuel Tank and the Booster to the Earth Atmosphere

Automation and remote control, 2023-03, Vol.84 (3), p.211-225

2023

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Research on the development of the agricultural sector of the Northern zone: repair and maintenance of machines

IOP conference series. Earth and environmental science, 2022-02, Vol.996 (1), p.12030

2022

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Thermal Conductivity of Phase Changing Materials Doped with Carbon Nanotubes

Journal of physics. Conference series, 2020-12, Vol.1683 (3), p.32011

2020

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Optimizing Flight Trajectories for Space Vehicles with an Additional Fuel Tank. II

Automation and remote control, 2018-02, Vol.79 (2), p.311-326

2018

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A Thermal Accumulator Based on Phase-Change Materials

Doklady. a journal of the Russian Academy of Sciences. Physics, 2022-06, Vol.67 (6), p.169-172

2022

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Optimizing flight trajectories for space vehicles with an additional fuel tank. I

Automation and remote control, 2017-12, Vol.78 (12), p.2203-2210

2017

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New age datings of gabbroides of the Kershor complex (Polar Urals)

Doklady earth sciences, 2010-09, Vol.434 (1), p.1235-1239

2010

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Multilevel Governance and Resource Exchange: Votes, Budgets, Information

Polis (Moscow, Russia), 2021-01 (1), p.169

2021

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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

Automation and remote control, 2024-01, Vol.85 (1), p.15-34

2024

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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

Avtomatika i telemehanika, 2024-12 (1)

2024

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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 Spacecraft Motion

Cosmic research, 2003-05, Vol.41 (3), p.285-309

2003

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One optimization problem for trajectories of spacecraft rendezvous mission to a group of asteroids

Cosmic research, 2009-10, Vol.47 (5), p.426-437

2009

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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 limited thrust engine: II

Cosmic research, 2007-12, Vol.45 (6), p.523-534

2007

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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

Cosmic research, 2002-01, Vol.40 (1), p.81-104

2002

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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 limited thrust engine: I

Cosmic research, 2007-08, Vol.45 (4), p.339-347

2007

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First ACT global trajectory optimisation competition: Results found at Moscow State University

Acta astronautica, 2007-11, Vol.61 (9), p.758-762

2007

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About one problem of trajectory optimization

Cosmic research, 2008-06, Vol.46 (3), p.233-237

2008

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The transformation education concept in the digital ecosystem of a territorial production cluster

Informatika i obrazovanie, 2023-01, Vol.37 (6), p.5-11

2023

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On solving the problems of optimization of trajectories of many-revolution orbit transfers of spacecraft

Cosmic research, 2006-05, Vol.44 (3), p.258-267

2006

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Preparation of heat- and light-resistant dye from perylene-3,4,9,10-tetracarboxylic acid dianhydride and 3-aminopropyltriethoxysilane

Doklady. Chemistry, 2010-08, Vol.433 (2), p.194-198

2010

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Transformation of approaches in teaching information technologies to engineering students

Informatika i obrazovanie, 2023-09, Vol.38 (4), p.5-13

2023

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The fastest maneuvers of a spacecraft with a jet engine of a large limited thrust in a gravitational field in a vacuum

Cosmic research, 2000-03, Vol.38 (2), p.160-181

2000

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The origin of membranes

Paleontological journal, 2010-12, Vol.44 (7), p.860-869

Natochin, Yu. V.

2010

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Application of the Local Estimation Methods to Calculate the Radiant Intensity of a High-Temperature Jet

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

Spacecraft Transfer Optimization with Releasing the Additional Fuel Tank and the Booster to the Earth Atmosphere

Research on the development of the agricultural sector of the Northern zone: repair and maintenance of machines

Thermal Conductivity of Phase Changing Materials Doped with Carbon Nanotubes

Optimizing Flight Trajectories for Space Vehicles with an Additional Fuel Tank. II

A Thermal Accumulator Based on Phase-Change Materials

Optimizing flight trajectories for space vehicles with an additional fuel tank. I

New age datings of gabbroides of the Kershor complex (Polar Urals)

Multilevel Governance and Resource Exchange: Votes, Budgets, Information

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

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

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

One optimization problem for trajectories of spacecraft rendezvous mission to a group of asteroids

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

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 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

First ACT global trajectory optimisation competition: Results found at Moscow State University

About one problem of trajectory optimization

The transformation education concept in the digital ecosystem of a territorial production cluster

On solving the problems of optimization of trajectories of many-revolution orbit transfers of spacecraft

Preparation of heat- and light-resistant dye from perylene-3,4,9,10-tetracarboxylic acid dianhydride and 3-aminopropyltriethoxysilane

Transformation of approaches in teaching information technologies to engineering students

The fastest maneuvers of a spacecraft with a jet engine of a large limited thrust in a gravitational field in a vacuum

The origin of membranes

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