Summary

This satellite Attitude Determination and Control System (ADCS) is designed for CubeSats ranging from 1.5U, 2U, 3U, to 6U. A full set of attitude determination / actuator hardware and firmware is embedded. This subsystem combines 6 Fine Sun Sensors (FSS100 from Tensor Tech), 1 reaction sphere (RS100 from Tensor Tech), and a tactical grade gyroscope, to provide a pointing accuracy up to 0.2 deg (3-sigma) when the sun is capturable and 1 deg (3-sigma) when it is not. A GPS module can increase the attitude determination precision.

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Last updated: 2021-02-03

ADCS100 - Integrated ADCS with Reaction Sphere

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Specs

lead time
4 week
pointing accuracy
0.2 deg (with sun), 1 deg (no sun)
data interface
I2C, UART
power consumption
< 1 W
mass
< 400 g
maximum torque
1 mN m
angular momentum storage
10 mN m s

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