11   Artículos

 
en línea
Filipp Kozin, Mahdi Akhloumadi and Danil Ivanov    
In this paper, a planar air-bearing test bed with unmanned aerial vehicles (UAV) was used to test a microsatellite motion control system. The UAV mock-ups were controlled by four ventilator actuators that imitated the satellite thrusters and provided the... ver más
Revista: Drones    Formato: Electrónico

 
en línea
Kirill Chernov, Uliana Monakhova, Yaroslav Mashtakov, Shamil Biktimirov, Dmitry Pritykin and Danil Ivanov    
The paper presents a study of decentralized control for a satellite formation flying mission that uses differential lift and drag to enforce the relative positioning requirements. All spacecraft are equipped with large sunlight reflectors so that, given ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Danil Ivanov, Goncalo Amaro, Yaroslav Mashtakov, Mikhail Ovchinnikov and Anna Guerman    
A formation flying control algorithm using the Lorentz force for Low Earth Orbits to achieve a trajectory with required shape and size is proposed in the paper. The Lorentz force is produced as a result of interaction between the Earth?s magnetic field a... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Stepan Tkachev, Yaroslav Mashtakov, Danil Ivanov, Dmitry Roldugin and Mikhail Ovchinnikov    
In this paper, the study of stabilization accuracy of a satellite equipped with a set of reaction wheels (RW) is presented. The model of motion takes into account possible static and dynamic reaction wheel imbalances. Due to the complexity of the model, ... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Danil Ivanov, Uliana Monakhova, Anna Guerman and Mikhail Ovchinnikov    
A decentralized control algorithm for the construction of a tetrahedral configuration using differential lift and drag forces is proposed in this paper. Four 3U CubeSats launched in LEO are considered. Satellite attitude-controlled motion relative to the... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mahdi Akhloumadi and Danil Ivanov    
Relative motion control problem for capturing the tumbling space debris object is considered. Onboard thrusters and reaction wheels are used as actuators. The nonlinear coupled relative translational and rotational equations of motion are derived. The SD... ver más
Revista: Aerospace    Formato: Electrónico

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