Abstract A satellite equipped with a magnetic attitude control system and a pitch flywheel has been considered. The system performance in the transient mode has been investigated. The characteristic exponent of the system have been approximated for a satellite on a circumpolar orbit. In the steady-state mode of gravitational attitude, small motions are considered in the vicinity of equilibrium. The attitude accuracy has been analyzed. The algorithm of an arbitrary but given attitude of the satellite in the orbital plane has been investigated. A numerical simulation has been performed.
Motion of a satellite equipped with a pitch flywheel and magnetic coils in gravitational field
Cosmic Research ; 55 , 3
2017
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Lokalklassifikation TIB: | 770/3520/8000 |
Motion of a satellite equipped with a pitch flywheel and magnetic coils in gravitational field
Springer Verlag | 2017
|Springer Verlag | 2017
|Satellite Flywheel Final Report
NTIS | 1970
|Modal control of flywheel motion in magnetic bearings
Tema Archiv | 2001
|