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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
magnetorquer2.JPG
Startracker Magnetorquer
Reaction wheels
Magnetorquer1
Reaction wheels
Magnetorquer in structure

 

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