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Attitude Determination and Control

To fulfill the mission requirements an accurate attitude determination and control of the satellite is essential. Therefore, sensors (sunsensors, magnetometer, startracker) and actuators (reaction wheels, magnetorquer) are used to provide three-axis control.

magnetometer1.JPG sunsensor2.JPG
Magnetometer Sunsensor
Startracker Magnetorquer
Reaction wheels
Reaction wheels
Magnetorquer in structure


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