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Application of the Angular Independent Variable and Its Regularizing Transformation in the Problems of Optimizing Low-Thrust Trajectories

Cosmic research, 2019-09, Vol.57 (5), p.351-363

Petukhov, V. G.

2019

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Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets

Cosmic research, 2023-10, Vol.61 (5), p.418-430

2023

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Minimum-Thrust Transfers to the Moon

Cosmic research, 2022-12, Vol.60 (6), p.481-490

2022

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Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits

Cosmic research, 2019-09, Vol.57 (5), p.378-388

2019

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Optimization of Perturbed Spacecraft Trajectories Using Complex Dual Numbers. Part 2: Numerical Results

Cosmic research, 2021-11, Vol.59 (6), p.517-528

2021

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Optimization of Perturbed Spacecraft Trajectories Using Complex Dual Numbers. Part 1: Theory and Method

Cosmic research, 2021-09, Vol.59 (5), p.401-413

2021

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Designing Low-Energy Low-Thrust Flight to the Moon on a Temporary Capture Trajectory

Cosmic research, 2023-10, Vol.61 (5), p.380-393

2023

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Method of continuation for optimization of interplanetary low-thrust trajectories

Cosmic research, 2012-05, Vol.50 (3), p.249-261

Petukhov, V. G.

2012

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Problematic issues of spacecraft development for contactless removal of space debris by ion beam

Acta astronautica, 2021-04, Vol.181, p.569-578

2021

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Control of a service satellite during its mission on space debris removal from orbits with high inclination by implementation of an ion beam method

Acta astronautica, 2022-05, Vol.194, p.390-400

2022

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Filter Electrostatic Charging in Fuel Purification

Inorganic materials : applied research, 2020, Vol.11 (4), p.861-864

2020

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Joint Optimization of Control and Main Trajectory and Design Parameters of an Interplanetary Spacecraft with an Electric Propulsion System

Cosmic research, 2019-05, Vol.57 (3), p.188-203

2019

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A realistic concept of a manned Mars mission with nuclear–electric propulsion

Acta astronautica, 2015-11, Vol.116, p.299-306

2015

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Optimization of the interplanetary trajectories of spacecraft with a solar electric propulsion power plant of minimal power

Solar system research, 2016-12, Vol.50 (7), p.552-559

2016

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Quasioptimal control with feedback for multiorbit low-thrust transfer between noncoplanar elliptic and circular orbits

Cosmic research, 2011-04, Vol.49 (2), p.121-130

Petukhov, V. G.

2011

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Optimization of Multi-Orbit Transfers between Noncoplanar Elliptic Orbits

Cosmic research, 2004-05, Vol.42 (3), p.250-268

Petukhov, V G

2004

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Optimization of interplanetary trajectories for spacecraft with ideally regulated engines using the continuation method

Cosmic research, 2008-06, Vol.46 (3), p.219-232

Petukhov, V. G.

2008

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Application of the complex-dual algebra for solving the optimization problem of perturbed low-thrust trajectories

AIP Conference Proceedings, 2023, Vol.2549 (1)

2023

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Applications of electric propulsion in scientific space projects: Benefits, features, and implementation examples

Solar system research, 2012-12, Vol.46 (7), p.523-530

2012

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Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit

Cosmic research, 2009-06, Vol.47 (3), p.243-250

Petukhov, V. G.

2009

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Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets

Kosmic̆eskie issledovanija, 2023-09, Vol.61 (5), p.406-419

2023

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Joint Optimization of the Trajectory and the Main Parameters of an Electric Propulsion System

Procedia engineering, 2017, Vol.185, p.312-318

2017

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Designing Low-Energy Low-Thrust Flight to the Moon on a Temporary Capture Trajectory

Kosmic̆eskie issledovanija, 2023-09, Vol.61 (5), p.368-381

2023

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The thrust minimization problem and its applications

Cosmic research, 2015-07, Vol.53 (4), p.300-310

2015

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One Variant of Manned Mission to Mars with a Nuclear Electric Propulsion

International journal of space technology management and innovation, 2011-04, Vol.1 (2), p.1-17

2011

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Application of the Angular Independent Variable and Its Regularizing Transformation in the Problems of Optimizing Low-Thrust Trajectories

Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets

Minimum-Thrust Transfers to the Moon

Low-Energy Sub-Optimal Low-Thrust Trajectories to Libration Points and Halo-Orbits

Optimization of Perturbed Spacecraft Trajectories Using Complex Dual Numbers. Part 2: Numerical Results

Optimization of Perturbed Spacecraft Trajectories Using Complex Dual Numbers. Part 1: Theory and Method

Designing Low-Energy Low-Thrust Flight to the Moon on a Temporary Capture Trajectory

Method of continuation for optimization of interplanetary low-thrust trajectories

Problematic issues of spacecraft development for contactless removal of space debris by ion beam

Control of a service satellite during its mission on space debris removal from orbits with high inclination by implementation of an ion beam method

Filter Electrostatic Charging in Fuel Purification

Joint Optimization of Control and Main Trajectory and Design Parameters of an Interplanetary Spacecraft with an Electric Propulsion System

A realistic concept of a manned Mars mission with nuclear–electric propulsion

Optimization of the interplanetary trajectories of spacecraft with a solar electric propulsion power plant of minimal power

Quasioptimal control with feedback for multiorbit low-thrust transfer between noncoplanar elliptic and circular orbits

Optimization of Multi-Orbit Transfers between Noncoplanar Elliptic Orbits

Optimization of interplanetary trajectories for spacecraft with ideally regulated engines using the continuation method

Application of the complex-dual algebra for solving the optimization problem of perturbed low-thrust trajectories

Applications of electric propulsion in scientific space projects: Benefits, features, and implementation examples

Optimal multi-orbit trajectories for inserting a low-thrust spacecraft to a high elliptic orbit

Optimization of a Low-Thrust Heliocentric Trajectory between the Collinear Libration Points of Different Planets

Joint Optimization of the Trajectory and the Main Parameters of an Electric Propulsion System

Designing Low-Energy Low-Thrust Flight to the Moon on a Temporary Capture Trajectory

The thrust minimization problem and its applications

One Variant of Manned Mission to Mars with a Nuclear Electric Propulsion

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