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Orientation control method for a low-orbit satellite using a triaxial arrangement of magneto-couplers together with a triaxial magnetometer for ensuring the satellite is correctly aligned using the Earth's magnetic field
Orientation control method for a low-orbit satellite using a triaxial arrangement of magneto-couplers together with a triaxial magnetometer for ensuring the satellite is correctly aligned using the Earth's magnetic field
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机译:使用磁耦合器的三轴布置和三轴磁力计的低轨道卫星的方向控制方法,以确保使用地球磁场正确对准卫星
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摘要
Method in which magneto-couplers are used to create a magnetic moment that is co-linear with the command direction of the satellite. The latter is determined using the geomagnetic field in the satellite reference axes with the latter pointing in an ideal direction so that the magnetic command direction is permanently aligned with the instantaneous magnetic direction. Satellite angular position around the instantaneous magnetic direction is controlled using a kinematic moment.
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