The CubeSpace CubeADCS is a complete turn-key nanosatellite attitude determination and control solution for users aiming to rapidly develop satellites using flight-proven components. These systems combine a robust, radiation-tolerant flight computer, flight-proven ADCS algorithms and FDIR mechanisms, and other wide range of sensors and actuators.

For CubeSats requiring high-accuracy inertial pointing, CubeSpace offers a 3-Axis variant of its CubeADCS. CubeADCS 3-Axis uses three reaction wheels, one in each principal axis of the satellite, to do full 3-axis pointing and tracking. A variety of CubeSpace sensors can be integrated with the system depending on the nominal mission control modes and on the pointing accuracy required.

The system includes features such as TLM logging, sensor and actuator power control and FDIR, communication bus monitoring, SGP4 orbit propagation, as well as estimator and control algorithms for virtually all ADCS control modes. On top of the control modes available on the Y-Momentum CubeADCS, this 3-Axis adds the capability to perform a 3-axis pointing in any direction.