Summary

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

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Specs

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

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