Method of controlling the attitude of a satellite in low orbit

摘要

A method for controlling the attitude of a satellite placed in low orbit comprising in particular a step of generating at least three angular moments, a step of generating a magnetic moment, a step of measuring the surrounding magnetic field of the satellite relative to the earth and a step of controlling one or more angular moments and / or the magnetic moment in order to modify the attitude of the satellite as a function of the surrounding magnetic field measured. Figure 1