The Attitude Determination and Control System (ADCS) module is responsible for controlling on orbit motion and position of the satellite. Three mems IMU, GPS and 2D sun sensor ensure precise orientation determination while actuation is provided by three mangnetorquers. ADCS is able to operate with reaction wheels (not included).

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Last updated: 2021-06-24

Attitude Determination and Control System



290 g
98 mm
95 mm
23 mm
supply voltage
9 to 13 V
power consumption
180 mW (standby)
12 W (operational)
data interface


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