Satellite > Attitude > Integrated ADCS > ADCS100 - Integrated ADCS with Reaction Sphere
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.
Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. Please report any mistakes to us.
Last updated: 2021-02-03
ADCS100 - Integrated ADCS with Reaction Sphere
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
Export
