Title :
Rotational motion of a nanosatellite using onboard electromagnetic coils after collision with a solid high-speed particle
Author :
Lyubimov, V.V. ; Osipov, A.A. ; Semkin, N.D.
Author_Institution :
Dept. of Higher Math., SSAU, Samara, Russia
Abstract :
In this study, we model a collision of a nanosatellite with space debris or micrometeoroids, leading to rotational motion of a nanosatellite. We consider the problem of controlled reduction of acquired angular velocity of a nanosatellite. The control process is based on the use of three electromagnets.
Keywords :
artificial satellites; coils; meteoroids; space debris; angular velocity; control process; micrometeoroids; nanosatellite; onboard electromagnetic coils; rotational motion; solid high-speed particle collision; space debris; Angular velocity; Coils; Damping; Magnetomechanical effects; Mathematical model; Satellites; Space debris; coil; control; nanosatellite; rotation; space debris;
Conference_Titel :
Control and Communications (SIBCON), 2015 International Siberian Conference on
Conference_Location :
Omsk
Print_ISBN :
978-1-4799-7102-2
DOI :
10.1109/SIBCON.2015.7147298
