has been cited by the following article(s):
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[1]
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Lifetime Extension of Ultra Low-Altitude Lunar Spacecraft with Low-Thrust Propulsion System
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Aerospace,
2022 |
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[2]
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Mapping Long-Term Natural Orbits about Titania, a Satellite of Uranus
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Symmetry,
2022 |
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[3]
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Numerical Modeling of the Dynamics of Artificial Satellites of the Moon
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Solar System …,
2022 |
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[4]
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Long-Term Dynamics and Special Solutions of Lunar Orbiters
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2022 |
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[5]
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Climate Mitigation and Adaption Using Energy Generating Cubesat as a Tool
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2022 Integrated Communication …,
2022 |
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[6]
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Анализ динамической структуры вековых резонансов в окололунном орбитальном пространстве
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Вестник Томского …,
2022 |
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[7]
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ИССЛЕДОВАНИЕ ВЛИЯНИЯ ВЕКОВЫХ И ПОЛУВЕКОВЫХ РЕЗОНАНСОВ НА ДИНАМИКУ ОКОЛОЛУННЫХ ОБЪЕКТОВ
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… сплошных сред и …,
2022 |
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[8]
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ЧИСЛЕННОЕ МОДЕЛИРОВАНИЕ ОСОБЕННОСТЕЙ ДИНАМИКИ ОКОЛОЛУННЫХ ОБЪЕКТОВ
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… сплошных сред и …,
2021 |
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[9]
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INVESTIGATION OF THE INFLUENCE OF SECULAR AND HALF-SECULAR RESONANCES ON THE DYNAMICS OF NEAR-LUNAR OBJECTS
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Maxim Yu. Orlov National …,
2021 |
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[10]
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Numerical Modeling of the Special Features in the Dynamics of Near-Moon Objects
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2020 |
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[11]
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Study of the dynamic structure of the near-lunar orbital space
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2020 |
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[12]
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Анализ стабильности низких селеноцентрических орбит
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2020 |
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[13]
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Численная модель движения искусственных спутников Луны и возможности ее использования: магистерская диссертация по направлению подготовки …
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2020 |
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[14]
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Analysis of lifetime extension capabilities for CubeSats equipped with a low-thrust propulsion system for Moon missions
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2019 |
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[15]
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Основные особенности динамики окололунных объектов
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2019 |
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[16]
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Moon Mission Lifetime Analysis of a 2U CubeSat Equipped with Pulsed Plasma Thrusters; The Aoba-VELOX IV Mission Case
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2017 |
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[17]
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Moon mission lifetime analysis of a 2U CubeSat equipped with pulsed plasma thrusters: The Aoba-VELOX IV mission case
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2017 |
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[18]
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Potencial gravitacional lunar
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Repositório Institucional UNESP,
2015 |
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[19]
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Trajectory design for a very-low-thrust lunar mission.
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2013 |
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[20]
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RELATÓRIO PARCIAL
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2013 |
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[21]
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Trajectory Design for a Very-Low-Thrust Lunar Mission
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NULL
2012 |
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[22]
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Attitude and Orbit Control System for a 6U CubeSat Mission in Low Altitude Lunar Orbit using Low-Thrust Propulsion System
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ALARCON, M LATERZA
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[23]
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NUMERICAL MODELING OF THE DYNAMICS OF NEAR-LUNAR OBJECTS
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[1]
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Mapping Long-Term Natural Orbits about Titania, a Satellite of Uranus
Symmetry,
2022
DOI:10.3390/sym14040667
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[2]
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Lifetime Extension of Ultra Low-Altitude Lunar Spacecraft with Low-Thrust Propulsion System
Aerospace,
2022
DOI:10.3390/aerospace9060305
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[3]
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Numerical Modeling of the Dynamics of Artificial Satellites of the Moon
Solar System Research,
2022
DOI:10.1134/S0038094622040074
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[4]
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Low selenocentric orbits stability analysis
Engineering Journal: Science and Innovation,
2020
DOI:10.18698/2308-6033-2020-10-2023
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[5]
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Analysis of lifetime extension capabilities for CubeSats equipped with a low-thrust propulsion system for Moon missions
Acta Astronautica,
2019
DOI:10.1016/j.actaastro.2018.11.040
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