The invention discloses a
satellite posture all-round controlling method based on a
magnetic moment device and a
flywheel, relating to an all-round posture controlling method for completing a
satellite orbit-injection phase by using the
magnetic moment device and the
flywheel. The invention solves the problems of low reliability and short service life of the traditional
satellite posture all-round controlling technology. The satellite posture all-round controlling method comprises the following steps of: 1, setting controller parameters according to the requirement of a
control system; 2, measuring a geomagnetic
field intensity vector Bb, a satellite
angular velocity vector Wb and a solar
azimuth, and sending the measured data to a satellite controller; 3, calculating an expected control
moment vector Tm and a control
magnetic moment vector Mm, and sending the control magnetic
moment vector Mm to the magnetic moment device; 4, acquiring an effective solar
azimuth vector Alfa; 5, calculating a control input
moment vector Tw and sending to the
flywheel; and 6, jointly completing the satellite posture all-round control by the magnetic moment device according to the control magnetic moment vector Mm and the flywheel according to the control input moment vector Tw. The invention is suitable for the field of satellite posture control.