- 1 Spherical Motor serves as 3 single-axis reaction wheels and 3 torquers
- Environmental Tests following ESA QB50
- Sun sensor, and Tactical Grade Gyro Included
Our 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. Our subsystem combines six Fine Sun Sensors (FSS100 from Tensor Tech), one Reaction Sphere (RS100 from Tensor Tech), one gyroscope, and one magnetometer to provide a pointing accuracy up to 0.2 deg (3-sigma) when the sun is capturable and 1 deg (3-sigma) when the sun is not capturable. The input of GPS module data is required for attitude determination.
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Power Consumption: 1W
Pointing Accuracy: 0.2 deg
Angular Momentum Storage: 10 mNms
Maximum Torque: 1mNm
Interface: I2C, UART
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