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Many CubeSats use magnetic torquers for attitude control. Many of these same CubeSats use a magnetometer as the primary sensor for attitude determination. This results in a conflict where the actuators in the system corrupt the feedback measurements. Two common approaches to solve this problem are to physically separate the torquers and magnetometer by putting the magnetometer on a boom, or to separate...
Set the date range to filter the displayed results. You can set a starting date, ending date or both. You can enter the dates manually or choose them from the calendar.