Abstract The electrodynamic method of spacecraft attitude control is studied in an octupole geomagnetic field approximation. An analytical derivation is given for refined laws of control over spacecraft electrodynamic parameters, which ensure the required spacecraft guidance. Spacecraft equilibrium position is proved to be stable under continually acting disturbances. The effectiveness and practical feasibility of the proposed spacecraft attitude control method is confirmed by numerical analysis.
Electrodynamic control for spacecraft attitude stability in the geomagnetic field
Cosmic Research ; 52 , 6 ; 472-480
01.11.2014
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Electrodynamic control for spacecraft attitude stability in the geomagnetic field
Online Contents | 2014
|Spacecraft Attitude Rate Estimation from Geomagnetic Field Measurements
Online Contents | 2003
|Attitude stabilization of a rigid spacecraft in the geomagnetic field
Online Contents | 2007
|