| 摘要 |
<p>The correcting torque magnetically applied to a satellite to control at least its roll/yaw attitude is determined by establishing the direction of the rolling/yawing plane, wherein a correcting torque can be generated strictly in this plane, by the interaction of a magnetic moment produced on board in the plane of the pitch axis and of the earth's magnetic field with said magnetic field. A control law is used whose gains vary as a function of the local magnetic field of the earth to take into account the predetermined stresses exerted on the poles of the system.</p> |
